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Ariane 5

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Ariane 5 Original design of Ariane 5 with Hermes manned spaceplane and first production Ariane 5G. Credit: © Mark Wade

Status: Active. First Launch: 2016-06-18. Last Launch: 2016-10-05. Number: 2 .

Ariane 2010 Projected version of Ariane 5 with improvements in engine and materials.

Ariane 5 EC-B The ultimate evolved Ariane 5 funded as of the end of the millennium. A larger LOx/LH2 upper stage using the Vinci motor in place of the HM7B. The core remains the same. Result is an increase in GTO payload from 10.5 metric tons to 12.0 metric tons.

Ariane 5 FLS Partially reusable concept of 1988 using Ariane 5 core with twin reusable flyback boosters.

Ariane 5 RRL Partially reusable concept of 1993 using Ariane 5 core with flyback booster stages with Russian engines (RD-120 or RD-701).

Ariane 5ECA French orbital launch vehicle, first version of the evolved Ariane 5. The solid booster motors propellant load was increased by 2.43 metric tons and the case was welded, for a weight saving in dry mass of 1.9 metric tons. The core was powered by an improved Vulcain 2 engine. The oxygen-rich cycle of the engine allowed the oxygen bulkhead to be moved within the stage, resulting in a 15.2 metric ton increase in propellant in the core. A new LOx/LH2 upper stage, using the HM7B engine and oxygen tank from the Ariane 4 series, replaced the storable propellant EPS stage of earlier models. The result was an increase in payload to geosynchronous transfer orbit from 6 metric tons to 10.5 metric tons.

Ariane 5ES Version of the evolved Ariane 5 using a version of the EPS storable propellant stage instead of the new LOx/LH2 stage. Result was a payload to GTO of 8 metric tons. The use of the new Aestus restartable engine in the upper stage fitted the vehicle for space station logistics missions or launch of space probes requiring complex orbital maneuvers. Specifically designed to orbit ESA's Automated Transfer Vehicle (ATV) resupply vehicle for the International Space Station.

Ariane 5G Initial version of the Ariane 5, a bit too large for the main commercial geosynchronous communications satellite payloads.

Photo Gallery

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New Generation LVs From left: 3 versions of Atlas 5, 5 versions of Delta 4, 3 versions of Chinese NGLV, Ariane 5. Vertical scale is 10 m intervals. Credit: © Mark Wade

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• Preliminary design of all-new replacement of Ariane 4 launch vehicle begins. - . Nation: France.

• Full scale development of Ariane 5 launch vehicle authorised. - . Nation: France. The Ariane 5 was a completely new design, with a single-engine Lox/LH2 core stage flanked by two solid rocket boosters. Full scale development cost $ 8 billion..

• Cluster F1 - . Nation: Europe. Agency: ESA. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Cluster.

  The Cluster satellites were a series of sophisticated earth-observation platforms that were to be launched aboard the first Ariane 5. The explosion of the booster led to a costly setback for European space science. There were no back-up spacecraft. Some instruments may fly on other future satellites.

• Cluster F3 - . Nation: Europe. Agency: ESA. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Cluster.

• Cluster F4 - . Nation: Europe. Agency: ESA. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Cluster.

• Cluster F2 - . Nation: Europe. Agency: ESA. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Cluster.

• MAQSAT-H/TEAMSAT - . Payload: MAQSAT-H. Nation: Europe. Agency: ESA. Manufacturer: Kayser-Threde. Class: Technology. Type: Navigation technology satellite. Spacecraft: MAQSAT. USAF Sat Cat: 25023 . COSPAR: 1997-066A. Apogee: 26,504 km (16,468 mi). Perigee: 545 km (338 mi). Inclination: 7.60 deg. Period: 465.70 min. Dummy communications satellite instrumented to report the actual payload bay environment during launch. It included the TEAMSAT technology experiment payload, developed by ESTEC.

• MAQSAT-B/EPS - . Payload: MAQSAT-B. Nation: Europe. Agency: ESA. Manufacturer: Kayser-Threde. Class: Technology. Type: Navigation technology satellite. Spacecraft: MAQSAT. USAF Sat Cat: 25024 . COSPAR: 1997-066B. Apogee: 26,549 km (16,496 mi). Perigee: 541 km (336 mi). Inclination: 7.60 deg. Period: 466.40 min. Dummy satellite in the lower bay of the SPELTRA dual launch adapter..

• YES - . Payload: Young Engineers Satellite. Nation: Europe. Agency: ESA. Manufacturer: ESTEC. Class: Technology. Type: Navigation technology satellite. Spacecraft: YES. USAF Sat Cat: 25025 . COSPAR: 1997-066C. Apogee: 26,604 km (16,530 mi). Perigee: 558 km (346 mi). Inclination: 7.60 deg. Period: 467.70 min. Young Engineers Satellite with several technology experiments. Ejected from MAQSAT-H/TEAMSAT..

• Maqsat 3 - . Nation: France. Agency: ESA. Manufacturer: Kayser-Threde. Class: Technology. Type: Navigation technology satellite. Spacecraft: MAQSAT. USAF Sat Cat: 25503 . COSPAR: 1998-059A. Apogee: 35,491 km (22,053 mi). Perigee: 1,017 km (631 mi). Inclination: 7.50 deg. Period: 641.20 min.

  Maqsat 3 was an instrumentation package used to monitor performance of the Ariane 5 booster. At T+12:43 the Speltra adapter cover separated revealing Maqsat-3. At T+15:14 the EPS stage Aestus engine ignited and burned until T+31:00. At this point on a normal mission the satellite would separate from the EPS, but to avoid creating space debris Maqsat remained attached to the EPS. The EPS/Maqsat-3 was placed in a 1027 km x 35863 km x 7.0 degree geostationary transfer orbit.

• ARD - . Payload: Atmospheric Reentry Demonstrator. Nation: France. Agency: Arianespace. Program: ISS. Class: Technology. Type: Navigation technology satellite. Spacecraft: ARD. COSPAR: 1998-059S.

  The ARD was an 80 percent scale model of the Apollo Command Module, and a technology test for a possible International Space Station Crew Rescue Vehicle. Equipment included a TDRS satellite communications system; a GPS navigation system; 7 DASA 40 kgf hydrazine attitude control thrusters; a 2.8 m diameter heat shield; three 23 metre diameter parachutes, and a SARSAT recovery beacon. The ARD separated from the Ariane EPS upper stage at 12 minutes 2 seconds after launch. ARD and the EPC stage manoeuvred into a 1 km x 830 km orbit, guaranteeing re-entry at the end of the first orbit. The spacecraft splashed down in the Pacific at 3.69 degrees N, 153.35 degrees W, and was successfully recovered by the French Navy.

• XMM - . Mass: 3,764 kg (8,298 lb). Nation: Europe. Agency: ESA. Manufacturer: Friedrichshafen. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: XMM. USAF Sat Cat: 25989 . COSPAR: 1999-066A. Apogee: 104,406 km (64,874 mi). Perigee: 16,709 km (10,382 mi). Inclination: 62.50 deg. Period: 2,872.40 min. ESA's X-ray Multi-Mirror space observatory was the biggest science satellite ever built in Europe. Complementary in characteristics to NASA's Chandra satellite, the spacecraft were expected to make major new astronomical discoveries..

• Asiastar - . Payload: Eurostar 2000+. Mass: 2,778 kg (6,124 lb). Nation: Europe. Agency: Worldspace. Manufacturer: Toulouse. Program: Worldspace. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 2000. USAF Sat Cat: 26107 . COSPAR: 2000-016A. Apogee: 35,805 km (22,248 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  Direct Radio Broadcasting satelllite. First night launch of Ariane 5. Worldspace's second digital radio satellite. Joined Afristar in orbit with a mission of providing radio broadcasting to the developing world. Stationed at 105 deg E. Positioned in geosynchronous orbit at 105 deg E in 2000. As of 4 September 2001 located at 104.96 deg E drifting at 0.015 deg W per day. As of 2007 Mar 9 located at 104.99E drifting at 0.012W degrees per day.

• Insat 3B - . Mass: 2,778 kg (6,124 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Insat 2. Spacecraft: Insat 3. USAF Sat Cat: 26108 . COSPAR: 2000-016B. Apogee: 35,987 km (22,361 mi). Perigee: 35,931 km (22,326 mi). Inclination: 1.20 deg. Period: 1,444.90 min.

  Replaced the lost Insat 2D and carried a pure telecommunications payload of C, Ku and S band transponders. Stationed at 83 deg E. Positioned in geosynchronous orbit at 73 deg E in 2000. As of 5 September 2001 located at 83.07 deg E drifting at 0.014 deg W per day. As of 2007 Mar 11 located at 82.94E drifting at 0.012W degrees per day.

• Astra 2B - . Payload: Eurostar 2000+. Mass: 3,320 kg (7,310 lb). Nation: Europe. Agency: SES. Manufacturer: Toulouse. Program: Astra. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 2000. USAF Sat Cat: 26494 . COSPAR: 2000-054A. Apogee: 35,801 km (22,245 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  Direct Broadcasting satellite. Launch postponed from July 25. Astra 2B was an Astrium/Toulouse Eurostar 2000+ television broadcast satellite owned by the Luxembourg-based Societe Europeene de Satellites. The satellite was to be stationed at 28.2E to replace the German DFS Kopernikus. It carried 28 Ku-band transponders. By September 19 Astra 2B was in a 31,153 x 35,762 km x 0.3 deg orbit, approaching geosynchronous altitude. Stationed at 28 deg E. Positioned in geosynchronous orbit at 28 deg E in 2000. As of 20 August 2001 located at 28.50 deg E drifting at 0.011 deg E per day. As of 2007 Mar 10 located at 28.15E drifting at 0.017W degrees per day.

• GE 7 - . Payload: A2100A. Mass: 3,320 kg (7,310 lb). Nation: USA. Agency: GE Americom. Manufacturer: Lockheed. Program: Americom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 26495 . COSPAR: 2000-054B. Apogee: 35,797 km (22,243 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  Direct Broadcasting satellite. GE Americom satellite to provide cable TV distribution coverage to the USA. Equipped with 24 C-band transponders. Its dry mass was 912 kg and it carried 1023 kg of fuel at launch. The satellite is an A2100A model built by Lockheed Martin/Lockheed, the first lightweight A2100 with a mass about half that of earlier A2100 satellites. By September 19 GE 7 was in a 35,832 x 35,869 km x 0.1 deg orbit drifting over 146 deg W. Stationed at 137 deg W. Positioned in geosynchronous orbit at 137 deg W in 2000. As of 4 September 2001 located at 136.92 deg W drifting at 0.003 deg E per day. As of 2007 Mar 9 located at 137.03W drifting at 0.000E degrees per day.

• PAS 1R - . Mass: 4,758 kg (10,489 lb). Nation: USA. Agency: Panamsat. Manufacturer: El Segundo. Program: Panamsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 702. USAF Sat Cat: 26608 . COSPAR: 2000-072A. Apogee: 35,793 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

  First use of the ASAP-5 piggyback payload adapter. Communications satellite, stationed at 58 deg W. PAS 1R was a large Boeing Model 702 satellite with a dry mass of about 3000 kg (launch mass 4793 kg) and a solar panel span of 45m. It carried 36 C and 48 Ku-band transponders. PAS 1R was operated by Panamsat, whose fleet included the former Hughes Galaxy system. The PAS 1R, STRV 1c/1d, and AMSAT Phase 3D satellites were placed in orbit on a single Ariane launch. The EPS stage entered geostationary transfer orbit at 0134 GMT, followed by separation of the PAS 1R main payload. As of 4 September 2001 located at 45.03 deg W drifting at 0.016 deg W per day. As of 2007 Mar 1 located at 45.05W drifting at 0.023W degrees per day.

• STRV-1d - . Mass: 4,758 kg (10,489 lb). Nation: UK. Agency: Arianespace. Manufacturer: Farnborough. Class: Technology. Type: Navigation technology satellite. Spacecraft: STRV. USAF Sat Cat: 26611 . COSPAR: 2000-072D. Apogee: 39,282 km (24,408 mi). Perigee: 605 km (375 mi). Inclination: 7.10 deg. Period: 708.30 min.

  STRV-1c and 1d were small satellites built by the DERA (former Royal Aircraft Establishment), Farnborough, England. Mass was around 95 kg each. STRV-1d carries an NRL Space Test Program experiment (S97-2), a camera, and technology and computer experiments.

• STRV-1c - . Mass: 4,758 kg (10,489 lb). Nation: UK. Agency: Arianespace. Manufacturer: Farnborough. Class: Technology. Type: Navigation technology satellite. Spacecraft: STRV. USAF Sat Cat: 26610 . COSPAR: 2000-072C. Apogee: 39,218 km (24,368 mi). Perigee: 636 km (395 mi). Inclination: 6.34 deg. Period: 707.65 min.

  The two small STRV cubes were then ejected from the Ariane EPS stage ASAP-5 secondary payload structure at 0141 GMT. STRV-1c and 1d were small satellites built by the DERA (former Royal Aircraft Establishment), Farnborough, England. Mass was around 95 kg each. STRV-1c performed accelerated life testing of new components and materials in the high radiation environment of geosynchronous transfer orbit.

• AMSAT-Oscar-40 - . Mass: 4,758 kg (10,489 lb). Nation: Germany. Agency: AMSAT. Program: Oscar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Oscar. USAF Sat Cat: 26609 . COSPAR: 2000-072B. Apogee: 58,650 km (36,440 mi). Perigee: 1,167 km (725 mi). Inclination: 7.50 deg. Period: 1,146.50 min.

  The long-delayed Phase 3D amateur radio satellite, built by AMSAT-DL (Germany), was renamed AMSAT-Oscar-40 (AO-40) once launched. It carried an MBB S400 liquid engine (the backup engine for the Galileo Jupiter probe) and a variety of amateur radio payloads in L, S, C, X, V, U and K bands, as well as an ammonia arcjet thruster and a laser communications experiment. The satellite was the largest amateur satellite orbited to date and the first to feature deployable solar panels. Mass was 397 kg dry. The PAS 1R, STRV 1c/1d, and AMSAT Phase 3D satellites were placed in orbit on a single Ariane launch. At 0149 GMT the SBS cylindrical adapter which connected PAS-1R to AMSAT was jettisoned; 50 seconds later AMSAT separated from the EPS upper stage. Thereafter the spacecraft could not be contacted. Finally telemetry was received from after two weeks of silence, confirming that the satellite was still functioning.

• Astra 2D - . Mass: 1,414 kg (3,117 lb). Nation: Europe. Agency: SES. Manufacturer: El Segundo. Program: Astra. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 376. USAF Sat Cat: 26638 . COSPAR: 2000-081A. Apogee: 35,895 km (22,304 mi). Perigee: 35,886 km (22,298 mi). Inclination: 0.20 deg. Period: 1,441.41 min.

  Astra 2D was a Boeing 376HP spin-stabilised satellite, with a dry mass of around 700 kg. It was owned by the Luxembourg-based company SES and was to broadcast to the British Isles. Astra 2D was in a 292 x 35835 km x 2.2 deg transfer orbit on December 22 and was subsequently boosted into geosynchronous orbit by its Star 30 apogee kick motor. The 825 kg (dry mass) satellite carried 16 Ku-band transponders to provide direct-to-home voice, video, and data transmissions to Britain and neighboring countries after parking over 28.2 deg-E longitude. Positioned in geosynchronous orbit at 28 deg E in 2001 As of 3 September 2001 located at 28.17 deg E drifting at 0.014 deg E per day. As of 2007 Mar 10 located at 28.17E drifting at 0.014W degrees per day.

• GE 8 / Aurora 3 - . Payload: A2100A. Mass: 2,015 kg (4,442 lb). Nation: USA. Agency: GE Americom. Manufacturer: Lockheed. Program: Americom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 26639 . COSPAR: 2000-081B. Apogee: 35,795 km (22,241 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.00 deg. Period: 1,436.25 min.

  GE 8 was a C-band TV and data distribution satellite for GE Americom. The Lockheed Martin A2100A spacecraft had a launch mass of 2015 kg, a dry mass of 919 kg, and was equipped with 24 C-band transponders. By December 26 GE 8 had reached an 18656 x 35760 km x 0.4 deg orbit on its way to geostationary orbit. It was jointly owned by AT&T Alascom for Alaskan communications, and was also called Aurora III. Americom and Alascom were originally both RCA subsidiaries. Alascom continued to use the Americom network while GE operated the satellite. The 2.2 tonne (with fuel) spacecraft carried 24 C-band transponders to provide voice, video, and broadband data communications to the contiguous USA, Alaska, and the Caribbean after parking over 139 deg-W longitude. Positioned in geosynchronous orbit at 146 deg W in 2001 As of 5 September 2001 located at 139.01 deg W drifting at 0.000 deg W per day. As of 2007 Mar 11 located at 139.03W drifting at 0.003E degrees per day.

• LDREX - . Mass: 1,414 kg (3,117 lb). Nation: Japan. Agency: NASDA. Class: Technology. Type: Navigation technology satellite. Spacecraft: LDREX. Decay Date: 2010-03-21 . USAF Sat Cat: 26640 . COSPAR: 2000-081C. Apogee: 30,257 km (18,800 mi). Perigee: 241 km (149 mi). Inclination: 2.40 deg. Period: 527.50 min.

  Ariane V138's EPS upper stage carried an ASAP5 small payload attachment ring with a special camera system and the LDREX experimental antenna for Japan's NASDA space agency. LDREX (Large-scale Deployable Reflector EXperiment) was a 6-m diameter antenna which was to have deployed 40 minutes after launch, to test the deployment mechanism for the larger antenna to be used on the ETS-8 satellite. After the test the antenna was to have been jettisoned. However the experiment failed and no deployment or jettison took place.

• Eutelsat W1R / Eurobird - . Payload: Spacebus 3000B2. Mass: 3,050 kg (6,720 lb). Nation: Europe. Agency: Eutelsat. Manufacturer: Cannes. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 26719 . COSPAR: 2001-011A. Apogee: 35,798 km (22,243 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.00 deg. Period: 1,436.00 min.

  Launch delayed from March 2. Eurobird was a Spacebus 3000B3 built by Alcatel (Cannes). It was the 18th member of the European Eutelsat consortium's geosynchronous constellation and carried 24 Ku-band transponders to provide broad bandwidth and high power direct-to-home transmissions to enable digital entertainment and internet connections. The three tonne (with fuel) satellite was to be parked over 28.5 deg-E longitude, replacing the aging Copernicus (Kopernikus (DFS 3), 1992-066A). Dry mass was probably around 1300 kg. The satellite had an Astrium S400 bipropellant engine. Positioned in geosynchronous orbit at 28 deg E in 2001 As of 4 September 2001 located at 28.50 deg E drifting at 0.005 deg W per day. As of 2007 Mar 11 located at 28.52E drifting at 0.000W degrees per day.

• BSAT-2a - . Mass: 3,050 kg (6,720 lb). Nation: Japan. Agency: BSAT. Manufacturer: Cannes. Program: BSAT. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 26720 . COSPAR: 2001-011B. Apogee: 35,807 km (22,249 mi). Perigee: 35,764 km (22,222 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  BSAT-2a was a Japanese geosynchronous communications spacecraft and the second Orbital STAR-class television broadcasting satellite. Its launch mass was 1317 kg; dry mass was 535 kg. The satellite had a Thiokol Star 30CBP solid apogee motor. The new BSTAR STAR-class satellites are a new design replacing the earlier Starbus type satellite of which only one (Cakrawarta 1) was launched. BSAT Corp. (Broadcasting Satellite System Corp.) earlier launched HS-376 satellites BSAT 1a and 1b, replacing the government's BS series which began Japanese direct broadcast services in 1978. The satellite was to be parked over 110 deg-E longitude to provide direct-to-home voice, video and internet communications. Positioned in geosynchronous orbit at 110 deg E in 2001 As of 5 September 2001 located at 109.82 deg E drifting at 0.018 deg W per day. As of 2007 Mar 11 located at 109.92E drifting at 0.009W degrees per day.

• Artemis - . Mass: 3,105 kg (6,845 lb). Nation: Europe. Agency: ESA. Manufacturer: Alenia. Class: Technology. Type: Communications technology satellite. Spacecraft: Italsat. USAF Sat Cat: 26863 . COSPAR: 2001-029A. Apogee: 32,586 km (20,247 mi). Perigee: 32,451 km (20,164 mi). Inclination: 1.10 deg. Period: 1,272.40 min.

  Artemis was a European Space Agency satellite designed to test new communications technologies. The Ariane 510 vehicle failed to reach its correct orbit. The solid boosters and main stage worked as planned and put the EPS upper stage in the planned near-suborbital trajectory. The EPS stage then fired but the Aestus engine failed to reach full thrust and cut off 1 minute early. Instead of the planned 858 x 35853 km orbit, only a 592 x 17528 km orbit was reached. The 3.1 tonne (with fuel), 2.5 kW spacecraft carried two pairs of ion engines and had adequate xenon propellant for those engines to reach geosynchronous altitude. This was the first ever rescue of a satellite mission using electric propulsion. The satellite reached its operational orbit in 31 January 2003.using the four German RITA electric xenon thrusters. Artemis could then function as originally planned, as there remained sufficient chemical propellant for 10 years' operation. Artemis was to provide voice and data communications between mobile phones in Europe and North America, and act as a relay satellite between low-Earth orbiters and ground stations. Eventually, as part of the planned EGNOS system (to be operational by about 2010) it was to provide navigation/location determination as an independent European counterpart to the GPS and GLONASS fleets. As of 2007 Mar 11 located at 21.40E drifting at 0.001W degrees per day.

• BSAT-2b - . Mass: 3,105 kg (6,845 lb). Nation: Japan. Agency: BSAT. Manufacturer: Alenia. Program: BSAT. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. Decay Date: 2014-01-28 . USAF Sat Cat: 26864 . COSPAR: 2001-029B. Apogee: 17,400 km (10,800 mi). Perigee: 659 km (409 mi). Inclination: 2.90 deg. Period: 317.20 min.

  BSAT-2b was planned as a geosynchronous television broadcast satellite for the Japanese B-SAT company. It used Orbital's Star 1 bus and had a launch mass of 1298 kg. It carried a Thiokol Star 30 solid apogee motor and a set of station-keeping thrusters with 200 kg of propellant. A propulsion problem in the final stage of rocket stranded the satellite at a much lower altitude than planned. Since BSAT 2B carried only a soild propellant apogee kick motor, it was unable to maneuver itself to a useful orbit.

• Envisat - . Mass: 7,991 kg (17,617 lb). Nation: Europe. Agency: Arianespace. Class: Earth. Type: Civilian Radarsat. Spacecraft Bus: SPOT-4. Spacecraft: Envisat. USAF Sat Cat: 27386 . COSPAR: 2002-009A. Apogee: 785 km (487 mi). Perigee: 783 km (486 mi). Inclination: 98.60 deg. Period: 100.50 min.

  This launch was the first Ariane 5 to use the 17-m Long Fairing and the first to launch north from Kourou. The booster placed the European Space Agency's Envisat polar platform in orbit. The flight profile was quite different from earlier Ariane 5 GTO launches where the EPC core stage usually reached a marginal orbit. In this case EPC separation at 350 km high 10 min after launch. The stage was on a -2610 x 651 km x 93.8 deg orbit, reaching apogee around 0125 UTC and reentering north of Ellesmere Island at about 0136 UTC. The EPS final stage with Envisat only achieved a positive perigee at 22 minutes after launch, with a circular 790 km sun-synchronous orbit reached at 25 min after launch. ESA reported the booster put the satellite to within 20 m of the desired orbital position.

• Stellat 5 - . Payload: Spacebus 3000B3. Mass: 4,050 kg (8,920 lb). Nation: France. Agency: Stellat. Manufacturer: Cannes. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 27460 . COSPAR: 2002-035A. Apogee: 35,807 km (22,249 mi). Perigee: 35,767 km (22,224 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

  Launch delayed from late June. Stellat-5 was an Alcatel Spacebus 3000B3 with a dry mass of 1805 kg and 2245 kg of propellant. The satellite carried Ku-band and C-band transponders, and was a joint venture between France Telecom and Europeon.Star which was to provide 2-way internet access and video transmission from 5 deg W. Stellat-5 was colocated with France Telecom's Telecom 2C. As of 2007 Mar 10 located at 4.99W drifting at 0.000E degrees per day.

• NStar c - . Mass: 4,050 kg (8,920 lb). Nation: Japan. Agency: Stellat. Manufacturer: Cannes. Program: N-STAR. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 27461 . COSPAR: 2002-035B. Apogee: 35,801 km (22,245 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

  Launch delayed from late June. The N-Star c satellite was an S-band satellite for mobile telephone communications for NTT DoCoMo of Japan. N-Star c had a communications payload built by Lockheed Martin and used the Star 2 bus from Orbital. The small Star 2 satellite had a dry mass around 800 kg and was the first flight of a new Orbital hydrazine/nitrogen tetroxide liquid apogee propulsion system with a 500N thrust apogee engine developed by Japan's IHI. As of 2007 Mar 9 located at 135.92E drifting at 0.012W degrees per day.

• Atlantic Bird 1 - . Mass: 2,700 kg (5,900 lb). Nation: Europe. Agency: Eutelsat. Manufacturer: Alenia. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Italsat. USAF Sat Cat: 27508 . COSPAR: 2002-040A. Apogee: 35,787 km (22,236 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  Launch delayed from August 27. Atlantic Bird was a European (EUTELSAT) geostationary communications spacecraft. The 2.7-ton (1550 kg dry with 1150 propellant), 5 kW satellite was to provide voice, video, and Internet services to Europe and the eastern part of America through its 24 transponders after being parked over 12.5° W. As of 2007 Mar 10 located at 12.49W drifting at 0.006W degrees per day.

• Meteosat 8 - . Payload: MSG 1. Mass: 2,010 kg (4,430 lb). Nation: Europe. Agency: Eutelsat. Manufacturer: Alenia. Class: Earth. Type: Weather satellite. Spacecraft: MSG. USAF Sat Cat: 27509 . COSPAR: 2002-040B. Apogee: 35,790 km (22,230 mi). Perigee: 35,784 km (22,235 mi). Inclination: 1.80 deg. Period: 1,436.10 min.

  Launch delayed from August 27. MSG 1 (Meteosat Second Generation 1) was a European (EUMETSAT consortium) geostationary weather satellite. After first being parked over 10° E longitude for six months it was later to be moved to zero degree longitude. As of 2007 Mar 7 located at 3.50W drifting at 0.015W degrees per day.

• Hot Bird 7 - . Payload: Eurostar 2000+. Mass: 3,350 kg (7,380 lb). Nation: Europe. Agency: Eutelsat. Manufacturer: Friedrichshafen. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 2000. Maiden flight of Ariane 5 EC-A. Delayed from October, November 20 and 28. Hot Bird 7, a Eutelsat geostationary communications satellite, was lost in the failed first flight of the Ariane 5 EC-A. Value of the lost satellite was Euro 250 million..

• Stentor - . Payload: Modified Spacebus 3000B3. Mass: 2,210 kg (4,870 lb). Nation: France. Agency: Eutelsat. Manufacturer: Friedrichshafen. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000.

  Maiden flight of Ariane 5 EC-A. Delayed from October, November 20 and 28. Stentor, a French experimental geostationary direct broadcast communications satellite, was lost in the failed first flight of the Ariane 5 EC-A. Value of the lost satellite was Euro 388 million.

• Insat 3A - . Mass: 2,958 kg (6,521 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Insat 2. Spacecraft: Insat 3. USAF Sat Cat: 27714 . COSPAR: 2003-013A. Apogee: 35,802 km (22,246 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Return to flight of Ariane 5G after grounded following Ariane 5EC-A failure. Launch delayed from February 24, April 8, 2003. Satellite also had meteorological instruments. As of 2007 Mar 10 located at 93.48E drifting at 0.009W degrees per day..

• Galaxy 12 - . Mass: 1,792 kg (3,950 lb). Nation: USA. Agency: PanAmSat. Manufacturer: OSC. Program: Galaxy. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 27715 . COSPAR: 2003-013B. Apogee: 35,791 km (22,239 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.10 deg. Period: 1,436.10 min. As of 2007 Mar 11 located at 125.09W drifting at 0.001W degrees per day..

• Optus and Defence 1 - . Mass: 4,725 kg (10,416 lb). Nation: Australia. Agency: Arianespace. Program: Aussat. Class: Communications. Type: Military communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 27830 . COSPAR: 2003-028A. Apogee: 35,803 km (22,246 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  Satellite jointly owned by Singtel Optus Pty and the Australian Dept. of Defense. Previous satellites in the series were purely civilian and didn't carry the dedicated defence communications equipment. Prime contractor for the satellie was Mitsubishi, using a Loral FS-1300 bus with UHF, X-band and Ka-band communications transponders. As of 2007 Mar 11 located at 109.87E drifting at 0.009W degrees per day.

• BSAT-2c - . Payload: Star 1. Mass: 1,298 kg (2,861 lb). Nation: Japan. Agency: BSAT. Manufacturer: OSC. Program: BSAT. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 27831 . COSPAR: 2003-028B. Apogee: 35,802 km (22,246 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.00 deg. Period: 1,436.10 min. As of 2007 Mar 9 located at 155.98E drifting at 0.008W degrees per day..

• Insat 3E - . Mass: 2,750 kg (6,060 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Insat 2. Spacecraft: Insat 3. USAF Sat Cat: 27951 . COSPAR: 2003-043E. Apogee: 35,803 km (22,246 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.0900 deg. Period: 1,436.06 min.

  The 440 Newton Liquid Apogee Motor (LAM) took the satellite from its Geosynchronous Transfer Orbit (GTO) of 649 km perigee and 36,000 km apogee with an orbital inclination of 7 deg. The LAM was fired for a total duration of 121 minutes in three phases on September 29, September 30 and October 1. A total velocity of 1460 m/sec was added by LAM at apogee. INSAT-3E had 1592 kg propellant at the time of its injection into GTO by Ariane-5 launch vehicle on September 28. After orbit raising operations, it had 510 kg of propellant remaining that was sufficient to arrest the drift and park it at its orbital slot as well as maintain the satellite in its orbit and controlling its orientation during its design life of more than 12 years. After the completion of the third apogee motor firing, the Solar Arrays and Antennae of INSAT-3E were deployed. The Sun tracking solar array of INSAT-3E had a total area of 29.6 sq m and it is designed to generate 2.9 kW (BoL) of power in orbit. The satellite had two deployable antennas and one fixed antenna. The satellite was expected to reach its final orbital slot of 55 deg E and be put into operation by November 2003. As of 2007 Mar 9 located at 54.97E drifting at 0.001W degrees per day. In 2014 the satellite was decommissioned; it began to slowly drift off station in late March and its orbit was lowered on April 4 to 35579 x 35693 km, drifting two degrees east per day.

• SMART-1 - . Mass: 370 kg (810 lb). Nation: Europe. Agency: ESA. Class: Technology. Type: Space probe technology. Spacecraft: SMART-1. COSPAR: 2003-043x. Apogee: 35,803 km (22,246 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.0900 deg. Period: 1,436.06 min.

  European Space Agency satellite which was to use ion drive and gravity assists to reach lunar orbit. The spacecraft made its third lunar resonance gravity assist on October 12, 2004. The continued gravitational effect of the Moon resulted in lunar capture on November 15, 2004,, when SMART-1 entered a 4962 x 51,477 km orbit around the Moon inclined at 81 degrees to the lunar equator.

• E-Bird - . Payload: BSS-376HP. Mass: 1,525 kg (3,362 lb). Nation: Europe. Agency: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 376. USAF Sat Cat: 27948 . COSPAR: 2003-043A. Apogee: 35,790 km (22,230 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.0500 deg. Period: 1,436.06 min.

  Last flight of the Ariane 5G. Launch delayed from July 15, August 22 and 28, September 3. The e-Bird was to service high-speed access networks providing both forward and return links via satellite. The spacecraft carried 20 active Ku-band transponders, each powered by a 33-watt traveling wave tube amplifier. The Ku-band transponders were connected to four spot beams that would provide coverage over Europe and Turkey. The spacecraft was to operate at 33 degrees East longitude, and had a contract life of 10 years.

• Rosetta - . Mass: 3,065 kg (6,757 lb). Nation: Europe. Agency: ESA. Manufacturer: Friedrichshafen. Class: Comet. Type: Comet probe. Spacecraft: Rosetta. USAF Sat Cat: 28169 . COSPAR: 2004-006A. Launch delayed from January 13, 2003, February 26 and 27, 2004..

• Anik F2 - . Mass: 5,950 kg (13,110 lb). Nation: Canada. Agency: Telesat. Manufacturer: El Segundo. Program: Anik. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 702. USAF Sat Cat: 28378 . COSPAR: 2004-027A. Apogee: 38,333 km (23,818 mi). Perigee: 33,253 km (20,662 mi). Inclination: 0.20 deg. Period: 1,436.40 min. Delayed from May, July 9, 13, 16 and 17. Heaviest single payload to GTO to that date. As of 2007 Mar 11 located at 111.09W drifting at 0.004W degrees per day..

• Helios 2A - . Mass: 4,200 kg (9,200 lb). Nation: France. Agency: DGA. Manufacturer: EADS Astrium. Program: Helios. Class: Surveillance. Type: Military surveillance satellite. Spacecraft Bus: SPOT-5A-5B. Spacecraft: Helios 2. USAF Sat Cat: 28492 . COSPAR: 2004-049A. Apogee: 690 km (420 mi). Perigee: 688 km (427 mi). Inclination: 98.08 deg. Period: 98.39 min. First of two new-generation French military surveillance satellites. Last flight of Ariane 5G model. Launch delayed from December 10..

• Parasol - . Mass: 125 kg (275 lb). Nation: France. Agency: CNES. Manufacturer: EADS Astrium. Class: Surveillance. Type: SIGINT. Spacecraft: Myriade. USAF Sat Cat: 28498 . COSPAR: 2004-049G. Apogee: 673 km (418 mi). Perigee: 659 km (409 mi). Inclination: 98.08 deg. Period: 97.91 min.

  Parasol carried a wide-field imaging radiometer/polarimeter called POLDER (Polarization and Directionality of the Earth's Reflectances), designed in partnership with the LOA atmospheric optics laboratory in Lille (CNRS-USTL). POLDER was designed to improve the knowledge of the radiative and microphysical properties of clouds and aerosols by measuring the directionality and polarization of light reflected by the Earth-atmosphere system.

• Essaim 1 - . Mass: 120 kg (260 lb). Nation: France. Agency: DGA. Manufacturer: EADS Astrium. Class: Surveillance. Type: SIGINT. Spacecraft: Myriade. USAF Sat Cat: 28494 . COSPAR: 2004-049C. Apogee: 673 km (418 mi). Perigee: 663 km (411 mi). Inclination: 98.08 deg. Period: 97.96 min.

  The Essaim demonstrator was a system of several micro-satellites (Essaim means 'swarm' in French) for 'analysis of the electro-magnetic environment of the Earth's surface' (electronic intelligence). DGA, the French Ministry of Defence's procurement agency, developed the project. The system also comprised a ground control segment and a ground station for data processing. It was called a 'demonstrator' since the mission's objective was to assess the operational capability of such a system, paving the way for the next generation. The Essaim satellites were based on EADS Astrium's Myriade multipurpose micro-satellite. In early 2000, the DGA awarded the contract for the development, manufacturing of this turnkey system of micro-satellites and associated ground segment. Under the contract, EADS Astrium was also responsible for personnel training and system operations during the three-year life duration of the programme.

• Essaim 2 - . Mass: 120 kg (260 lb). Nation: France. Agency: DGA. Manufacturer: EADS Astrium. Class: Surveillance. Type: SIGINT. Spacecraft: Myriade. USAF Sat Cat: 28495 . COSPAR: 2004-049D. Apogee: 664 km (412 mi). Perigee: 657 km (408 mi). Inclination: 98.10 deg. Period: 98.00 min.

• Essaim 3 - . Mass: 120 kg (260 lb). Nation: France. Agency: DGA. Manufacturer: EADS Astrium. Class: Surveillance. Type: SIGINT. Spacecraft: Myriade. USAF Sat Cat: 28496 . COSPAR: 2004-049E. Apogee: 667 km (414 mi). Perigee: 654 km (406 mi). Inclination: 98.10 deg. Period: 98.00 min.

• Essaim 4 - . Mass: 120 kg (260 lb). Nation: France. Agency: DGA. Manufacturer: EADS Astrium. Class: Surveillance. Type: SIGINT. Spacecraft: Myriade. USAF Sat Cat: 28497 . COSPAR: 2004-049F. Apogee: 670 km (410 mi). Perigee: 651 km (404 mi). Inclination: 98.10 deg. Period: 98.00 min.

• Nanosat 01 - . Mass: 20 kg (44 lb). Nation: Spain. Agency: Arianespace. Manufacturer: INTA. Class: Technology. Type: Navigation technology satellite. Spacecraft: Nanosat 01. USAF Sat Cat: 28493 . COSPAR: 2004-049B. Apogee: 666 km (413 mi). Perigee: 658 km (408 mi). Inclination: 98.10 deg. Period: 98.00 min. Experimental nanosat built by the Spanish space agency (INTA)..

• XTAR-EUR - . Mass: 3,631 kg (8,004 lb). Nation: Spain. Agency: ESA. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28542 . COSPAR: 2005-005A. Apogee: 35,794 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  Return to flight of Ariane 5 EC-A after booster failure on first launch. Delayed from April, June, September 28, October 28, November 3 and 8, 2004; and February 11, 2005. XTAR-EUR was a Spanish X-band military communications satellite operated by Hisdesat/XTAR of Spain. It had a dry mass of 1412 kg and 2219 kg of propellant. As of 2007 Mar 8 located at 28.95E drifting at 0.006W degrees per day.

• Maqsat-B2 - . Mass: 3,622 kg (7,985 lb). Nation: Europe. Agency: ESA. Manufacturer: Kayser-Threde. Class: Technology. Type: Navigation technology satellite. Spacecraft: Maqsat. Decay Date: 2012-12-03 . USAF Sat Cat: 28543 . COSPAR: 2005-005B. Apogee: 35,409 km (22,002 mi). Perigee: 258 km (160 mi). Inclination: 6.70 deg. Period: 624.90 min. Maqsat was a test payload built by Kayser-Threde to study the Ariane 5ECA launch environment. Remained attached to the upper stage..

• SLOSHSAT - . Payload: SLOSHSAT-FLEVO. Mass: 127 kg (279 lb). Nation: Netherlands. Agency: ESA. Class: Technology. Type: Navigation technology satellite. Spacecraft: SLOSHSAT. USAF Sat Cat: 28544 . COSPAR: 2005-005C. Apogee: 35,723 km (22,197 mi). Perigee: 268 km (166 mi). Inclination: 6.80 deg. Period: 631.20 min. Test satellite to study the sloshing of fluids in zero gravity, developed by the Netherlands Aerospace Laboratory. Equipped with a tank with 33.5 liters of water and an attitude control system..

• Ipstar 1 - . Payload: Thaicom 4, LS-1300SX. Mass: 6,486 kg (14,299 lb). Nation: Thailand. Agency: Shinawat. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28786 . COSPAR: 2005-028A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Ariane 5GS version maiden flight. Launch delayed from July 8 and 11, 2005. Heaviest geosynchronous transfer orbit payload to date. As of 2007 Mar 11 located at 119.46E drifting at 0.009W degrees per day..

• Galaxy 15 - . Mass: 2,033 kg (4,481 lb). Nation: USA. Agency: PanAmSat. Manufacturer: OSC. Program: Galaxy. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 28884 . COSPAR: 2005-041A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Slated to provide satellite television services to the United States market. As of 2007 Mar 10 located at 132.99W drifting at 0.009W degrees per day..

• Syracuse 3A - . Payload: Spacebus 4000B3. Mass: 3,725 kg (8,212 lb). Nation: France. Agency: DGA. Manufacturer: Alenia. Program: Syracuse. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 28885 . COSPAR: 2005-041B. Apogee: 35,803 km (22,246 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Syracuse 3A French military communications satellite. Launch delayed from mid-February, March 15, April 14, May 31, 2005. As of 2007 Mar 10 located at 47.00E drifting at 0.010E degrees per day..

• Telkom 2 - . Mass: 1,975 kg (4,354 lb). Nation: Indonesia. Agency: PT Telkom. Program: Palapa. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 28902 . COSPAR: 2005-046A. Apogee: 35,794 km (22,241 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.10 deg. Period: 1,436.20 min. Satellite's launch delayed from April 14, May 31, October 27, November 10 and 12, 2005, for technical problems. As of 2007 Mar 11 located at 118.00E drifting at 0.013W degrees per day..

• Spaceway 2 - . Mass: 6,116 kg (13,483 lb). Nation: USA. Agency: DirecTV. Manufacturer: El Segundo. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 702. USAF Sat Cat: 28903 . COSPAR: 2005-046B. Apogee: 35,788 km (22,237 mi). Perigee: 35,785 km (22,235 mi). Period: 1,436.10 min.

  Heaviest total commercial GTO payload to that date. Qualification flight for the Ariane 5 EC-A version. Launch delayed from June 25 due to launch vehicle problems. Spaceway 2 launch delayed from April for problems with the satellite. As of 2007 Mar 10 located at 99.24W drifting at 0.010W degrees per day.

• Insat 4A - . Mass: 3,081 kg (6,792 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-3K. USAF Sat Cat: 28911 . COSPAR: 2005-049A. Apogee: 35,798 km (22,243 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

  Delayed from late July 2005. Launch delayed from August 23, October, November 14 and 30, December 8, 16 and 20. Dry mass 1385 kg. The satellite was equipped with Ku-band and C-band transponders and would join other Insats in providing telecommunications and television services to the Indian subcontinent. After three engine burns the satellite reached geostationary altitude over the Indian Ocean at 04:30 GMT on 26 December, then deployed its solar arrays. As of 2007 Mar 11 located at 83.00E drifting at 0.006W degrees per day.

• Meteosat 9 - . Payload: MSG 2. Mass: 2,034 kg (4,484 lb). Nation: Europe. Agency: Eumetsat. Manufacturer: Alenia. Class: Earth. Type: Weather satellite. Spacecraft: MSG. USAF Sat Cat: 28912 . COSPAR: 2005-049B. Apogee: 35,793 km (22,240 mi). Perigee: 35,779 km (22,231 mi). Inclination: 1.50 deg. Period: 1,436.10 min. Delayed from mid-February, March 15, June 2005. Meteosat Second Generation spin-stabilized weather satellite. As of 2007 Mar 10 located at 0.11W drifting at 0.024W degrees per day..

• Spainsat - . Payload: LS-1300. Mass: 3,683 kg (8,119 lb). Nation: Spain. Agency: Hisdesat. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28945 . COSPAR: 2006-007A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Spainsat was to provide secure X and Ku band communications for the Spanish defense ministry. It had a dry mass of 1467 kg and a solar panel span of 31.4m. As of 2007 Mar 10 located at 29.99W drifting at 0.010W degrees per day..

• Hot Bird 7A - . Payload: Spacebus 3000B3. Mass: 4,100 kg (9,000 lb). Nation: Europe. Agency: Eutelsat. Manufacturer: Alenia. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 28946 . COSPAR: 2006-007B. Apogee: 35,806 km (22,248 mi). Perigee: 35,767 km (22,224 mi). Inclination: 0.30 deg. Period: 1,436.10 min. Hot Bird 7A had a dry mass of 1740 kg and a solar panel span of 36.9m. As of 2007 Mar 9 located at 13.03E drifting at 0.010E degrees per day..

• Satmex 6 - . Payload: LS-1300. Mass: 5,465 kg (12,048 lb). Nation: Mexico. Agency: SatMex. Manufacturer: Palo Alto. Program: Morelos. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 29162 . COSPAR: 2006-020A. Apogee: 35,794 km (22,241 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. The satellite had a dry mass of 2310 kg and a hybrid C-band and Ku-band telecom payload for telecom and internet service in Mexico and the rest of North and Latin America As of 2007 Mar 11 located at 113.03W drifting at 0.002W degrees per day..

• Thaicom 5 - . Payload: Spacebus 3000A. Mass: 2,766 kg (6,097 lb). Nation: Thailand. Agency: Shinawat. Manufacturer: Alenia. Program: Thaicom. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 29163 . COSPAR: 2006-020B. Apogee: 36,036 km (22,391 mi). Perigee: 35,388 km (21,989 mi). Inclination: 0.10 deg. Period: 1,432.30 min. The satellite had a dry mass of 1220 kg and a payload designed for C/Ku-band telecom and TV transmission in the Asia-Pacific Region. It was to replace Thaicom 3. As of 2007 Mar 10 located at 78.52E drifting at 0.004W degrees per day..

• JCSAT 10 - . Payload: A2100AXS. Mass: 4,048 kg (8,924 lb). Nation: Japan. Agency: JSAT. Manufacturer: Lockheed. Program: JCSAT. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 29272 . COSPAR: 2006-033A. Apogee: 35,793 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Ku/C-band television broadcasting satellite for the Japanese market; mass 1858 kg dry. As of 2007 Mar 11 located at 128.01E drifting at 0.012W degrees per day..

• Syracuse 3B - . Payload: Spacebus 4000B3. Mass: 3,750 kg (8,260 lb). Nation: France. Agency: DGA. Manufacturer: Alenia. Program: Syracuse. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 29273 . COSPAR: 2006-033B. Apogee: 35,796 km (22,242 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. SHF and EHF military communications links for the French military. As of 2007 Mar 9 located at 5.21W drifting at 0.004W degrees per day..

• DirecTV 9S - . Mass: 8,180 kg (18,030 lb). Nation: USA. Agency: DirecTV. Manufacturer: Palo Alto. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 29494 . COSPAR: 2006-043A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Addition to DirecTV's direct broadcast television constellation. Carried 52 high-power Ku-band transponders and 2 Ka-band transponders. As of 2007 Mar 11 located at 101.13W drifting at 0.009W degrees per day..

• Optus D1 - . Payload: Star-2. Nation: Australia. Agency: Optus. Manufacturer: OSC. Program: Aussat. Class: Communications. Type: Military communications satellite. Spacecraft: Star bus. USAF Sat Cat: 29495 . COSPAR: 2006-043B. Apogee: 35,797 km (22,243 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.0400 deg. Period: 1,436.09 min. Direct television broadcast to the Australian market. As of 2007 Mar 7 located at 159.99E drifting at 0.005W degrees per day..

• LDREX 2 - . Nation: Japan. Agency: JAXA. Class: Technology. Type: Navigation technology satellite. Spacecraft: LDREX. Decay Date: 2010-09-30 . USAF Sat Cat: 29496 . COSPAR: 2006-043C. Apogee: 26,980 km (16,760 mi). Perigee: 227 km (141 mi). Inclination: 7.20 deg. Period: 468.50 min. LDREX-2 was attached to the upper stage. It deployed a 6.5-meter antenna design planned for the later ETS-8 satellite.

• WildBlue 1 - . Mass: 4,735 kg (10,438 lb). Nation: USA. Agency: Arianespace. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 29643 . COSPAR: 2006-054A. Apogee: 35,792 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0200 deg. Period: 1,436.09 min.

  Broadband internet satellite, using the Ka-band satellite. Dry mass 2000 kg. At separation of the Ariane core the stack was in a -1282 km x 233 km x 6.9 deg suborbital trajectory. The ESC-A upper stage fired to put the satellites in a geostationary transfer orbit of 265 km x 35700 km x 2.0 deg. As of 2007 Mar 11 located at 111.14W drifting at 0.004W degrees per day.

• AMC-18 - . Payload: A2100A. Mass: 2,081 kg (4,587 lb). Nation: USA. Agency: SES Americom. Manufacturer: Lockheed. Program: Americom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 29644 . COSPAR: 2006-054B. Apogee: 35,789 km (22,238 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0100 deg. Period: 1,436.09 min. C-band cable television distribution satellite with a dry mass of 918 kg. As of 2007 Mar 11 located at 104.94W drifting at 0.006W degrees per day..

• Skynet 5A - . Payload: Eurostar 3000S. Mass: 4,635 kg (10,218 lb). Nation: UK. Agency: Paradigm. Manufacturer: EADS Astrium. Program: Skynet. Class: Communications. Type: Military communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 30794 . COSPAR: 2007-007B. Apogee: 35,800 km (22,200 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Skynet 5A was launched by Paradigm Secure Communications as part of its turnkey contract to provide a secure communications satellite network to the British military and NATO..

• Insat 4B - . Mass: 3,035 kg (6,691 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-3K. USAF Sat Cat: 30793 . COSPAR: 2007-007A. Apogee: 35,808 km (22,250 mi). Perigee: 35,766 km (22,223 mi). Inclination: 0.00 deg. Period: 1,436.10 min. ISRO communications satellite with C and Ku band channels, and a dry mass of 1335 kg.

• Astra 1L - . Payload: A2100AXS. Mass: 4,497 kg (9,914 lb). Nation: Luxembourg. Agency: SES. Manufacturer: Lockheed. Program: Astra. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 31306 . COSPAR: 2007-016A. Apogee: 35,788 km (22,237 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.10 deg. Period: 1,436.00 min.

  Astra 1L provided direct-to-home broadcast services to Europe from its location at 19.2º East. It also strengthened the SES in-orbit backup system, extended fleet coverage from the Canary Islands eastwards up to the Russian border, and allowed Astra 2C to be moved from 19.2º East to 28.2º to fulfill high capacity demand from the U.K. and Ireland. Astra 1L was equipped with 29 Ku + 2 Ka active transponders, which would be reduced to 27 active transponders after its first five years of operation.

• Galaxy 17 - . Payload: Spacebus 3000B3. Mass: 4,100 kg (9,000 lb). Nation: USA. Agency: Intelsat. Manufacturer: Alenia. Program: Galaxy. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 31307 . COSPAR: 2007-016B. Apogee: 35,789 km (22,238 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.10 deg. Period: 1,436.10 min. C/Ku-band satellite for cable television relay in the United States..

• Spaceway 3 - . Mass: 6,075 kg (13,393 lb). Nation: USA. Agency: Hughes. Manufacturer: El Segundo. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 702. USAF Sat Cat: 32018 . COSPAR: 2007-036A. Apogee: 35,788 km (22,237 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.0200 deg. Period: 1,436.12 min. Satellite launched for Hughes Network Systems, with a Ka-band payload for space-based internet. Mass 3655 kg dry..

• BSAT-3A - . Payload: A2100A. Mass: 1,967 kg (4,336 lb). Nation: Japan. Agency: BSAT. Manufacturer: Lockheed. Program: BSAT. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 32019 . COSPAR: 2007-036B. Apogee: 35,826 km (22,261 mi). Perigee: 35,746 km (22,211 mi). Inclination: 0.10 deg. Period: 1,436.00 min. Satllite launched for the Japan Broadcasting Satellite Systems Corp. (BSAT) with a Ku-band television payload. Mass 930 kg dry..

• Optus D-2 - . Mass: 2,400 kg (5,200 lb). Nation: Australia. Agency: Optus. Manufacturer: OSC. Program: Aussat. Class: Communications. Type: Military communications satellite. Spacecraft: Star bus. USAF Sat Cat: 32252 . COSPAR: 2007-044A. Apogee: 35,889 km (22,300 mi). Perigee: 35,862 km (22,283 mi). Inclination: 0.00 deg. Period: 1,440.70 min.

  Ku-band satellite designed to deliver television, internet, communications, and data services to Australia and New Zealand. After deployment of the two satellites, the EPS third stage made a brief burn at 23:28 GMT to make the first in-flight test the Aestus engine's restart capability. This was to be used in 2008 in the first launch of the ATV ISS resupply spacecraft.

• Intelsat IS-11 - . Mass: 2,400 kg (5,200 lb). Nation: USA. Agency: Intelsat. Manufacturer: OSC. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 32253 . COSPAR: 2007-044B. Apogee: 35,797 km (22,243 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.10 deg. Period: 1,436.10 min. C and Ku-band satellite designed to provide Atlantic region communications services..

• Skynet 5B - . Payload: Eurostar 3000S. Mass: 4,635 kg (10,218 lb). Nation: UK. Agency: Paradigm. Program: Skynet. Class: Communications. Type: Military communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 32294 . COSPAR: 2007-056B. Apogee: 35,789 km (22,238 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Skynet 5B was designed to provide communications services in the SHF and UHF bands to the UK Ministry of Defence..

• Star One C1 - . Payload: Spacebus 3000B3. Mass: 4,100 kg (9,000 lb). Nation: Brazil. Agency: Embratel. Program: Brasilsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 32293 . COSPAR: 2007-056A. Apogee: 35,780 km (22,230 mi). Perigee: 35,794 km (22,241 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Formerly named Brasilsat C1, the satellite was launched as part of a joint venture between several South American countries with Brazil's Embratel taking a lead role..

• Rascom-QAF-1 - . Payload: Spacebus 4000B3. Mass: 4,579 kg (10,094 lb). Nation: Mauritius. Agency: RascomStarQAF. Manufacturer: Alenia. Program: Rascom. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 32387 . COSPAR: 2007-063A. Apogee: 35,796 km (22,242 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.10 deg. Period: 1,436.00 min.

  African communications satellite with a hybrid Ku/C-band payload. Nominal owner RascomStarQAF of Port Louis, Mauritius, a subsidiary of the Regional African Satellite Communications Organization (RASCOM) based in Cote d'Ivoire. The mission and satellite control centers were located in Cameroun and Libya. The satellite was to provide voice, data and internet services throughout Africa. Ahelium leak in the propulsion system prevented use of the primary apogee motor. Reaction control motors were used instead to slowly move the satellite into geosynchronous orbit. The satellite was expected to reach its operating location, but with a shorter-than-planned operational lifetime.

• Horizons 2 - . Payload: Star-2. Mass: 2,350 kg (5,180 lb). Nation: Bermuda. Agency: Intelsat, JSAT. Manufacturer: OSC. Program: Horizons. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 32388 . COSPAR: 2007-063B. Apogee: 35,816 km (22,254 mi). Perigee: 35,815 km (22,254 mi). Inclination: 0.00 deg. Period: 1,437.50 min.

  Launched by Horizons Satellite Holdings LLC, a joint venture of Intelsat and the Japanese JSAT company. To be placed at 74 deg W to serve United States, eastern Canada, and the Caribbean with communication services using its 16-transmitter Ku-band communications payload.

• ATV-1 Jules Verne - . Mass: 19,012 kg (41,914 lb). Nation: France. Agency: Arianespace. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: ATV. Duration: 204.39 days. Decay Date: 2008-09-29 . USAF Sat Cat: 32686 . COSPAR: 2008-008A. Apogee: 343 km (213 mi). Perigee: 336 km (208 mi). Inclination: 51.60 deg. Period: 91.30 min.

  First launch of Europe's Automated Transfer Vehicle, a logistics vehicle designed for ISS resupply. The Ariane model 5ES launch vehicle, vehicle L528, had the enhanced EAP solid boosters and EPC core stage of the Ariane 5ECA, but with the new EPS-V upper stage with restart capability and a vehicle equipment bay instrument unit strengthened to carry the heavier LEO payload. Jules Verne carried 1300 kg of dry cargo, 302 kg of water and oxygen, and 860 kg of propellant to the ISS. For this test mission it had a dry mass of 10075 kg and 6475 kg of maneuvering propellant (in later missions the propellant could be thousands of kilograms less, in order to deliver more cargo).

  The EPS stage made its first burn and placed the stack into a 137 km x 260 km orbit at 04:20 GMT. The EPS restarted at 05:05, burned for 30-seconds, and released the ATV into a 254 km x 272 km orbit.

  Following extensive checkouts and maneuvering near the ISS, ATV Jules Verne docked at the aft end of ISS Zvezda module at 14:52 GMT on 3 April. While docked to the station, it was used several times to boost the station's orbit and to shift it in debris avoidance maneuvers. The ATV undocked from the ISS on 5 September and used a fuel-conserving 23 days to position itself for a safe re-entry over the South Pacific. Final destructive re-entry began at 13:30 GMT on 29 September.

• Vinasat 1 - . Payload: A2100A. Mass: 6,740 kg (14,850 lb). Nation: Vietnam. Agency: Arianespace. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 32767 . COSPAR: 2008-018A. Apogee: 35,789 km (22,238 mi). Perigee: 35,787 km (22,236 mi). Inclination: 0.00 deg. Period: 1,436.20 min. First satellite launched by Vietnam. The Vietnam Post and Telecom Corporation communications satellite was equipped with C and Ku band payloads..

• Star One C2 - . Payload: Spacebus 3000B3. Mass: 4,100 kg (9,000 lb). Nation: Brazil. Agency: Arianespace. Program: Brasilsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 32768 . COSPAR: 2008-018B. Apogee: 35,790 km (22,230 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Communications satellite owned by Brazilian operator Star One with C, Ku and X-band transponders.

• Skynet 5C - . Payload: Eurostar 3000S. Mass: 4,638 kg (10,225 lb). Nation: UK. Agency: Arianespace. Program: Skynet. Class: Communications. Type: Military communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 33055 . COSPAR: 2008-030A. Apogee: 35,801 km (22,245 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.60 deg. Period: 1,436.10 min.

• Turksat 3A - . Payload: Spacebus 4000B2. Mass: 3,110 kg (6,850 lb). Nation: Turkey. Agency: Arianespace. Program: Turksat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 33056 . COSPAR: 2008-030B. Apogee: 35,811 km (22,251 mi). Perigee: 35,761 km (22,220 mi). Inclination: 0.00 deg. Period: 1,436.00 min. Replacement for Turksat-1C, positioned at 42 deg E; 24 Ku-band transponders..

• Protostar 1 / Intelsat 5 - . Payload: Intelsat 5. Mass: 4,100 kg (9,000 lb). Nation: Bermuda. Agency: Arianespace. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 33153 . COSPAR: 2008-034A. Apogee: 35,793 km (22,240 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Originally Chinasat 8; sale cancelled due to new US export regulations. Sold to Protostar in 2006, still to serve Chinese market. After launch when Protostar closed down sold to Intelsat and entered service as Intelsat 5..

• Badr 6 - . Mass: 52 kg (114 lb). Nation: Pakistan. Agency: Arianespace. Class: Communications. Type: Military communications satellite. Spacecraft: Badr. USAF Sat Cat: 33154 . COSPAR: 2008-034B. Apogee: 35,801 km (22,245 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

• Superbird 7 - . Mass: 4,820 kg (10,620 lb). Nation: Japan. Agency: Arianespace. Program: Superbird. Class: Communications. Type: Civilian communications satellite. Spacecraft: DS2000. USAF Sat Cat: 33274 . COSPAR: 2008-038A. Apogee: 35,804 km (22,247 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Ku-band Mitsubishi Electric DS2000 class satellite for Japanese television broadcasting..

• AMC 21 - . Mass: 2,500 kg (5,500 lb). Nation: France. Agency: Arianespace. Program: Americom. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 33277 . COSPAR: 2008-038D. Apogee: 35,677 km (22,168 mi). Perigee: 276 km (171 mi). Inclination: 2.10 deg. Period: 630.40 min. Ku-band satellite for SES Americom's North American services, using an Orbital Star 2 bus and a Thales Alenia communications payload..

• Hot Bird 9 - . Mass: 4,880 kg (10,750 lb). Nation: France. Agency: Arianespace. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 33459 . COSPAR: 2008-065A. Apogee: 35,792 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Ku-band satellite slated to replace Hot Bird 3 at 13 deg E..

• Eutelsat W2M - . Mass: 3,460 kg (7,620 lb). Nation: France. Agency: Arianespace. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-3K. USAF Sat Cat: 33460 . COSPAR: 2008-065B. Apogee: 35,843 km (22,271 mi). Perigee: 35,735 km (22,204 mi). Inclination: 0.10 deg. Period: 1,436.20 min. Ku-band satellite designed to operate at 10 deg E. It used the Indian Insat I3K bus and was the first foreign sale of an Indian-built satellite. It made it to geosynchronous orbit but suffered a power system and was written off eight days after launch..

• NSS 9 - . Mass: 2,400 kg (5,200 lb). Nation: Netherlands. Agency: Arianespace. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 33749 . COSPAR: 2009-008A. Apogee: 35,793 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

• Hot Bird 10 - . Mass: 4,875 kg (10,747 lb). Nation: Europe. Agency: Arianespace. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 33750 . COSPAR: 2009-008B. Apogee: 35,804 km (22,247 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

• Spirale A - . Mass: 117 kg (257 lb). Nation: France. Agency: Arianespace. Class: Surveillance. Type: SIGINT. Spacecraft: Myriade. USAF Sat Cat: 33751 . COSPAR: 2009-008C. Apogee: 35,693 km (22,178 mi). Perigee: 631 km (392 mi). Inclination: 1.80 deg. Period: 637.60 min. Demonstrator to prove infrared sensors designed to detect ballistic missile launches and other military targets..

• Spirale B - . Mass: 117 kg (257 lb). Nation: France. Agency: Arianespace. Class: Surveillance. Type: SIGINT. Spacecraft: Myriade. USAF Sat Cat: 33752 . COSPAR: 2009-008D. Apogee: 35,681 km (22,171 mi). Perigee: 641 km (398 mi). Inclination: 1.80 deg. Period: 637.60 min.

• Herschel - . Mass: 3,400 kg (7,400 lb). Nation: Europe. Agency: Arianespace. Class: Astronomy. Type: Infrared astronomy satellite. Spacecraft: Herschel. USAF Sat Cat: 34937 . COSPAR: 2009-026A.

  Carried Far Infra Red and Submillimeter Telescope. After completing a successful mission, the spacecraft was sent into solar orbit and was deactivated. Herschel departed L2 on 1 April 2013 and was turned off on 17 June in a 1.04 AU x 1.06 AU x 0.19 deg inclination solar orbit.

• Planck - . Mass: 1,940 kg (4,270 lb). Nation: Europe. Agency: Arianespace. Class: Astronomy. Type: Microwave astronomy satellite. Spacecraft: Planck. USAF Sat Cat: 34938 . COSPAR: 2009-026B.

  Cosmic background radiation anisotropy satellite, carried a telescope with a primary mirror of 1.5 meter in size. Mission was to measure the fine structure of the temperature of the cosmic microwave background radiation over the whole sky, leading to a better understanding of conditions at the time of the big bang. After completing a successful mission, the spacecraft was sent into solar orbit and was deactivated. Planck departed L2 on 14 August 2013 and was turned off on 23 October in a 1.00 AU x 1.10 AU x 0.1 deg inclination solar orbit.

• Terrestar-1 - . Mass: 6,910 kg (15,230 lb). Nation: USA. Agency: Arianespace. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 35496 . COSPAR: 2009-035A. Apogee: 35,790 km (22,230 mi). Perigee: 35,783 km (22,234 mi). Inclination: 5.90 deg. Period: 1,436.10 min. Heaviest communications satellite to date; equipped with an 18-meter deployable antenna for S-band mobile communications..

• JCSAT 12 - . Payload: A2100AXS. Mass: 4,000 kg (8,800 lb). Nation: France. Agency: Arianespace. Program: JCSAT. Class: Communications. Type: Communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 35755 . COSPAR: 2009-044A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

• Optus D3 - . Payload: Star-2.4. Nation: France. Agency: Arianespace. Program: Aussat. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 35756 . COSPAR: 2009-044B. Apogee: 35,800 km (22,200 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

• COMSATBw-1 - . Payload: Spacebus 3000B2. Mass: 2,440 kg (5,370 lb). Nation: France. Agency: Arianespace. Program: COMSATBw. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 35942 . COSPAR: 2009-054A. Apogee: 35,807 km (22,249 mi). Perigee: 35,765 km (22,223 mi). Inclination: 0.10 deg. Period: 1,436.10 min. German military communications satellite. Dry mass 1040 kg..

• Amazonas 2 - . Mass: 5,465 kg (12,048 lb). Nation: France. Agency: Arianespace. Program: Hispasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 35943 . COSPAR: 2009-054B. Apogee: 35,794 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Commercial broadcast satellite for North and South America..

• NSS 12 - . Mass: 5,620 kg (12,380 lb). Nation: France. Agency: Arianespace. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 36032 . COSPAR: 2009-058A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.00 deg. Period: 1,436.10 min. C- and Ku-band communications satellite stationed at 57 deg E..

• Thor 6 - . Payload: Spacebus 4000B2. Mass: 3,050 kg (6,720 lb). Nation: France. Agency: Arianespace. Program: Thor Comsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 36033 . COSPAR: 2009-058B. Apogee: 35,793 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Direct broadcast satellite stationed at 1 deg W..

• Helios 2B - . Mass: 4,200 kg (9,200 lb). Nation: France. Agency: Arianespace. Program: Helios. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: SPOT-5A-5B. USAF Sat Cat: 36124 . COSPAR: 2009-073A. Apogee: 680 km (420 mi). Perigee: 680 km (420 mi). Inclination: 98.00 deg. French military surveillance satellite..

• Astra 3B - . Mass: 5,471 kg (12,061 lb). Nation: Luxembourg. Agency: Arianespace. Program: Astra. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 36581 . COSPAR: 2010-021A. Apogee: 35,807 km (22,249 mi). Perigee: 35,765 km (22,223 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Communications satellite with 52 Ku-band transponders; stationed at 23.5 deg E..

• ComsatBW-2 - . Payload: Spacebus 3000B2. Mass: 2,440 kg (5,370 lb). Nation: Germany. Agency: Arianespace. Program: COMSATBw. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 36582 . COSPAR: 2010-021B. Apogee: 35,792 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.00 deg. Period: 1,436.10 min. German military communications satellite..

• Coms 1 - . Mass: 2,400 kg (5,200 lb). Nation: Korea South. Agency: Arianespace. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 36744 . COSPAR: 2010-032A. Apogee: 35,789 km (22,238 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Communication, Ocean and Meteorological Satellite. Weather, oceanography, and communications payloads..

• Arabsat 5A - . Mass: 4,800 kg (10,500 lb). Nation: Arab States. Agency: Arianespace. Program: Arabsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 36745 . COSPAR: 2010-032B. Apogee: 35,789 km (22,238 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Communications satellite with 16 C-band and 24 Ku-band transponders, stationed at 30.5 deg E..

• Nilesat 201 - . Payload: Spacebus 4000B2. Mass: 3,200 kg (7,000 lb). Nation: Egypt. Agency: Arianespace. Program: Nilesat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 36830 . COSPAR: 2010-037A. Apogee: 35,804 km (22,247 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Ku-band/Ka-band direct broadcasting satellite..

• Rascom QAF 1R - . Payload: RascomQAF-1R. Mass: 3,050 kg (6,720 lb). Nation: Nigeria. Agency: Arianespace. Program: Rascom. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 36831 . COSPAR: 2010-037B. Apogee: 35,804 km (22,247 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Ku and C band transponders to provide telecommunications, broadcasting and internet service to Africa for the Regional African Satellite Communications Organization..

• Eutelsat W3B - . Payload: Spacebus 4000. Mass: 5,370 kg (11,830 lb). Nation: Europe. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 37206 . COSPAR: 2010-056A. Apogee: 35,769 km (22,225 mi). Perigee: 262 km (162 mi). Inclination: 1.80 deg. Period: 631.90 min.

• Bsat 3B - . Payload: A2100A. Mass: 2,060 kg (4,540 lb). Nation: Japan. Program: BSAT. Class: Communications. Type: Communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 37207 . COSPAR: 2010-056B. Apogee: 35,801 km (22,245 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

• Hylas 1 - . Mass: 2,570 kg (5,660 lb). Nation: UK. Manufacturer: ISRO. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-2K. USAF Sat Cat: 37237 . COSPAR: 2010-065A. Apogee: 36,052 km (22,401 mi). Perigee: 35,522 km (22,072 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Ka band communications; 2570 kg loaded / 1125 kg unfuelled..

• Intelsat 17 - . Payload: Intelsat IS-17. Mass: 5,393 kg (11,889 lb). Nation: USA. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 37238 . COSPAR: 2010-065B. Apogee: 35,803 km (22,246 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Communications satellite to be stationed at 66 deg E over the Indian Ocean; 5540 kg loaded / 2393 kg unfuelled..

• Hispasat 1E - . Mass: 5,320 kg (11,720 lb). Nation: Spain. Agency: Hispasat. Program: Hispasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 37264 . COSPAR: 2010-070A. Apogee: 35,790 km (22,230 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Ku band communications; 5320 kg loaded / 2175 kg unfuelled..

• Koreasat 6 - . Payload: Star-2. Mass: 2,850 kg (6,280 lb). Nation: Korea South. Program: Koreasat. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 37265 . COSPAR: 2010-070B. Apogee: 35,827 km (22,261 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.00 deg. Period: 1,437.00 min. Ku band communications; 2850 kg loaded / 1150 kg unfuelled..

• ATV-2 Johannes Kepler - . Mass: 19,712 kg (43,457 lb). Nation: Europe. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-01M, Soyuz TMA-20. Spacecraft: ATV. Duration: 125.00 days. Decay Date: 2011-06-21 . USAF Sat Cat: 37368 . COSPAR: 2011-007A. Apogee: 347 km (215 mi). Perigee: 343 km (213 mi). Inclination: 51.60 deg. Period: 91.40 min. ISS resupply; second European Space Agency Automated Transfer Vehicle. Docked with the ISS Zvezda module on 25 February. Undocked on 21 June at 14:46 GMT. Retrofire the same day at 20:04 GMT sent it to burn up over the Pacific Ocean..

• Intelsat New Dawn - . Mass: 3,000 kg (6,600 lb). Nation: USA. Program: Intelsat. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 37392 . COSPAR: 2011-016A. Apogee: 35,786 km (22,236 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.10 deg. Period: 1,436.00 min.

  Communications satellite with C/Ku hybrid payload, and, to have been stationed at 32.8 deg E for coverage of Africa. New Dawn Satellite Co. Ltd. was a joint venture of Intelsat and Convergence Partners, Johannesburg, South Africa. Couldn't deploy its C-band antenna, although the Ku-band deployed and was functional.

• Yahsat 1A - . Mass: 5,965 kg (13,150 lb). Nation: UAE. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 37393 . COSPAR: 2011-016B. Apogee: 35,799 km (22,244 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Communications satellite, stationed at 52.5 deg E over the Indian Ocean, with C- and Ku-band payload for Al Yah Satellite Communications Company, Abu Dhabi..

• GSAT-8 - . Mass: 3,150 kg (6,940 lb). Nation: India. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-3K. USAF Sat Cat: 37605 . COSPAR: 2011-022A. Apogee: 35,816 km (22,254 mi). Perigee: 35,757 km (22,218 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Communications satellite with a GAGAN navigation payload..

• ST-2 - . Mass: 5,090 kg (11,220 lb). Nation: Japan. Program: Singapore, Taiwan. Class: Communications. Type: Civilian communications satellite. Spacecraft: DS2000. USAF Sat Cat: 37606 . COSPAR: 2011-022B. Apogee: 35,793 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Singapore-Taiwan 2 communications satellite with both C and Ku band transmitters..

• Astra 1N - . Mass: 5,350 kg (11,790 lb). Nation: Luxembourg. Program: Astra. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 37775 . COSPAR: 2011-041A. Apogee: 35,802 km (22,246 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.00 deg. Period: 1,436.00 min. Geosynchronous communications satellite to be stationed at 19.2 deg E for direct television broadcasting to Europe..

• BSAT-3C - . Payload: A2100A. Mass: 2,910 kg (6,410 lb). Nation: Japan. Program: BSAT. Class: Communications. Type: Communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 37776 . COSPAR: 2011-041B. Apogee: 35,791 km (22,239 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Japan's Broadcast Satellite Systems Corporation communications satellite..

• SES 2 - . Payload: Orbital Star 2.4. Mass: 3,200 kg (7,000 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 37809 . COSPAR: 2011-049A. Apogee: 35,796 km (22,242 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Communications satellite with 24 C-band and 24 Ku-band transponders, and a US Air Force infrared surveillance sensor experiment..

• Arabsat 5C - . Mass: 4,630 kg (10,200 lb). Nation: Arab States. Program: Arabsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 37810 . COSPAR: 2011-049B. Apogee: 35,790 km (22,230 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.10 deg. Period: 1,436.10 min. C-band/Ka-band communications satellite for television broadcast to Arab countries..

• ATV-3 Edoardo Amaldi - . Mass: 19,714 kg (43,461 lb). Nation: Europe. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: ATV. Duration: 194.00 days. Decay Date: 2012-10-03 . USAF Sat Cat: 38096 . COSPAR: 2012-010A. Apogee: 406 km (252 mi). Perigee: 392 km (243 mi). Inclination: 51.60 deg. Period: 92.50 min.

  European cargo station resupply spacecraft. Docked at the aft Zvezda port of the International Space Station on 28 March at 22:31 GMT. Its engines were used on 31 March and 5 April to reboost the ISS to a 387 km x 398 km orbit. Undocked at 21:44 GMT on 28 September and was deorbited over the Pacific at 23:42 GMT on 2 October, with loss of signal at 01:25 GMT on 3 October.

• JCSAT 13 - . Payload: A2100AXS. Mass: 4,528 kg (9,982 lb). Nation: Japan. Class: Communications. Type: Communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 38331 . COSPAR: 2012-023A. Apogee: 35,790 km (22,230 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Sky Perfect communications satellite..

• Vinasat 2 - . Payload: A2100A. Mass: 2,969 kg (6,545 lb). Nation: Vietnam. Class: Communications. Type: Communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 38332 . COSPAR: 2012-023B. Apogee: 35,788 km (22,237 mi). Perigee: 35,787 km (22,236 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Vietnam Posts and Telecom communications satellite..

• Echostar 17 - . Mass: 6,100 kg (13,400 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 38551 . COSPAR: 2012-035A. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.00 deg. Period: 1,436.10 min. High throughput Ku-band data satellite providing broadband Internet service across North America. Originally named Jupiter 1..

• Meteosat 10 - . Payload: MSG 3. Mass: 2,000 kg (4,400 lb). Nation: Europe. Class: Earth. Type: Weather satellite. Spacecraft: MSG. USAF Sat Cat: 38552 . COSPAR: 2012-035B. Apogee: 35,787 km (22,236 mi). Perigee: 35,784 km (22,235 mi). Inclination: 1.70 deg. Period: 1,436.00 min. Third Meteosat Second Generation weather satellite..

• Intelsat 20 - . Payload: Intelsat IS-20. Mass: 6,094 kg (13,434 lb). Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 38740 . COSPAR: 2012-043A. Apogee: 35,794 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

• Hylas 2 - . Mass: 3,311 kg (7,299 lb). Nation: UK. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 38741 . COSPAR: 2012-043B. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Carried 24 active Ka-band user beams and four gateway beams supporting corporate networking, broadband Internet access, and video distribution to Northern and Southern Africa, Eastern Europe and the Middle East..

• Astra 2F - . Mass: 5,968 kg (13,157 lb). Nation: Europe. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 38778 . COSPAR: 2012-051A. Apogee: 35,806 km (22,248 mi). Perigee: 35,768 km (22,225 mi). Inclination: 0.0600 deg. Period: 1,436.12 min. Astrium Eurostar 3000 communications satellite for SES of Luxembourg.

• GSAT-10 - . Mass: 3,435 kg (7,572 lb). Nation: Europe. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-3K. USAF Sat Cat: 38779 . COSPAR: 2012-051B. Apogee: 35,798 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0200 deg. Period: 1,436.12 min.

• Star One C3 - . Mass: 3,200 kg (7,000 lb). Nation: Brazil. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 38991 . COSPAR: 2012-062A. Apogee: 35,790 km (22,230 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.00 deg. Period: 1,436.00 min. An Orbital Geostar-2.4E for Star One of Rio de Janeiro, successor to Brasilsat..

• Eutelsat 21B - . Payload: Spacebus 4000C3. Mass: 5,012 kg (11,049 lb). Nation: Europe. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 38992 . COSPAR: 2012-062B. Apogee: 35,789 km (22,238 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.00 deg. Period: 1,436.10 min. A Thales Alenia Spacebus 4000C3 launched for Eutelsat SA of Paris.

• Skynet 5D - . Payload: Eurostar 3000S. Mass: 4,638 kg (10,225 lb). Nation: UK. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 39034 . COSPAR: 2012-075A. Apogee: 35,800 km (22,200 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.10 deg. Period: 1,436.00 min. British military communications..

• Mexsat-Bicentenario - . Payload: Star-2.4 Bus. Mass: 3,050 kg (6,720 lb). Nation: Mexico. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 39035 . COSPAR: 2012-075B. Apogee: 35,794 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Domestic Mexican Mobile Satellite Services using 12 Ku-band and 12 C-band transponders..

• Amazonas 3 - . Mass: 6,265 kg (13,811 lb). Nation: Spain. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 39078 . COSPAR: 2013-006A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0500 deg. Period: 1,436.07 min. Provides C and Ku band communications services to Brazil for Hispamar, a joint venture of Spain's Hispasat and Brazilian oil company Oi/Telemar..

• Azerspace - . Payload: Star-2 bus. Mass: 3,275 kg (7,220 lb). Nation: Azerbaijan. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 39079 . COSPAR: 2013-006B. Apogee: 35,793 km (22,240 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0100 deg. Period: 1,436.07 min. Operated by Azercosmos for the Azerbaijan Ministry of Communications and Information Technologies. Some capacity also used by Measat of Malaysia to provide services to Africa under the name Africasat-1A..

• ATV-4 Albert Einstein - . Mass: 19,870 kg (43,800 lb). Nation: Europe. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: ATV. Duration: 150.00 days. Decay Date: 2013-11-02 . USAF Sat Cat: 39175 . COSPAR: 2013-027A. Apogee: 421 km (261 mi). Perigee: 409 km (254 mi). Inclination: 51.65 deg. Period: 92.88 min. Delivered supplies to the ISS. Deorbited over the Pacific on 2 November 2013 at 11:28 GMT, entry loss of signal was at 12:04 GMT..

• Alphasat - . Payload: I-4A F4. Mass: 6,500 kg (14,300 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Alphabus. USAF Sat Cat: 39215 . COSPAR: 2013-038A. Apogee: 35,796 km (22,242 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.40 deg. Period: 1,436.09 min.

  Testbed communications satellite, a joint project between the European Space Agency and Inmarsat. Demonstrated a laser communications system and radio communications links in Q and V band; carried an operational extended L-band payloadto supplement Inmarsat's satellite broadband capacity. First flight of the new Astrium/Lampoldshausen 500N EAM (European Apogee Motor), a MON/MMH system with an Isp of about 325s. Dry mass iaround 3500 kg. By July 30 Alphasat was in a 25608 x 35809 km x 0.3 deg orbit.

• Insat 3D - . Mass: 2,090 kg (4,600 lb). Nation: India. Class: Earth. Type: Weather satellite. Spacecraft Bus: Insat 2. Spacecraft: Insat 3. USAF Sat Cat: 39216 . COSPAR: 2013-038B. Apogee: 35,793 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0700 deg. Period: 1,436.11 min. Indian Space Research Organization meteorological satellite, with 6-channel imager, 19-channel sounder, data relay system for Earth-based meteo stations, and a Satellite Aided Search and Rescue transponder. 935 kg dry mass..

• Eshail 1 - . Payload: EUTE 25B. Mass: 6,310 kg (13,910 lb). Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 39233 . COSPAR: 2013-044A. Apogee: 35,793 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0400 deg. Period: 1,436.12 min. Communications satellite jointly owned by Eutelsat and Eshailsat, a spinoff of ictQATAR, the Qatari Supreme Council of Information and Communications Technology. The satellite's is Arabic for Canopus. Stationed in geosynchronous orbit at 31.7 East..

• GSAT-7 - . Payload: Insat 4F. Mass: 2,650 kg (5,840 lb). Nation: India. Class: Communications. Type: Communications satellite. Spacecraft: I-2K. USAF Sat Cat: 39234 . COSPAR: 2013-044B. Apogee: 35,811 km (22,251 mi). Perigee: 35,762 km (22,221 mi). Inclination: 0.0400 deg. Period: 1,436.09 min. Communications satellite for the Indian Navy..

• ABS 2 - . Mass: 6,330 kg (13,950 lb). Nation: China. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 39508 . COSPAR: 2014-006A. Apogee: 35,801 km (22,245 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.0300 deg. Period: 1,436.10 min.

  Communications satellite for Hong-Kong-based Asia Broadcast Satellite. Stationed at 75 deg E, serving four continents: 6 dedicated high powered Ku-band beams for DTH services in the Eastern Hemisphere; C-band beams for Africa and SE Asia connectivity requirements; Ka-band beam targeting the MENA region for commercial and military applications.

• Athena-Fidus - . Payload: Spacebus-4000B2. Mass: 3,080 kg (6,790 lb). Nation: France. Spacecraft: Spacebus 4000. USAF Sat Cat: 39509 . COSPAR: 2014-006B. Apogee: 35,792 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0600 deg. Period: 1,436.10 min.

  Joint French/Italian military communications satellite for both military and civilian government communications; in France the civilian space agency CNES and the military procurement agency DGA were both responsible, while in Italy the corresponding Agenzia Spaziale Italiana and Segredifesa/DNA agencies were involved.

• Amazonas 4A - . Mass: 2,938 kg (6,477 lb). Nation: Spain. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 39616 . COSPAR: 2014-011A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0900 deg. Period: 1,436.12 min. Orbital GeoStar-2.4 for Hispasat of Spain. Placed in 260 x 35,690 km x 3.0 deg GTO orbit by launch vehicle; used its own propulsion system to reach geoscynchronous orbit..

• Astra 5B - . Mass: 5,724 kg (12,619 lb). Nation: SES. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 39617 . COSPAR: 2014-011B. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0600 deg. Period: 1,436.07 min. Airbus Defense and Space Eurostar 3000L communication satellite for SES. Placed in 260 x 35,690 km x 3.0 deg GTO orbit by launch vehicle; used its own propulsion system to reach geoscynchronous orbit..

• ATV-5 Georges Lemaitre - . Mass: 19,520 kg (43,030 lb). Nation: France. Agency: AE. Spacecraft: ATV. Duration: 201.00 days. Decay Date: 2015-02-15 . USAF Sat Cat: 40103 . COSPAR: 2014-044A. Apogee: 419 km (260 mi). Perigee: 413 km (256 mi). Inclination: 51.65 deg. Period: 92.89 min. ISS resupply mission. Arrived at the ISS on August 12, docking with Zvezda at 13:30 GMT. Undocked from the ISS Zvezda module at 13:42 GMT on February 14 2015 and was deorbited over the Pacific on February 15..

• Measat 3b - . Mass: 5,897 kg (13,000 lb). Nation: Malaysia. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 40147 . COSPAR: 2014-054B. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0400 deg. Period: 1,436.12 min. Communications satellite for Malaysia's Measat; part of the capacity is leased to NewSat (Melbourne) to be marketed as the Jabiru-2 payload..

• Optus 10 - . Mass: 3,970 kg (8,750 lb). Nation: Australia. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 40146 . COSPAR: 2014-054A. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Communications satellite owned by Singtel Optus, the Australian subsidiary of Singapore Telecom, with a Ku-band payload..

• Intelsat IS-30 - . Mass: 6,320 kg (13,930 lb). Nation: International. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 40271 . COSPAR: 2014-062A. Apogee: 35,796 km (22,242 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0100 deg. Period: 1,436.13 min. Ku-band payload leased to DirectTV as DLA-1 for broadcast to Latin America. Stationed in geosynchronous orbit at 95 deg west..

• ARSAT-1 - . Mass: 2,985 kg (6,580 lb). Nation: Argentina. Class: Communications. Type: Communications satellite. Spacecraft: ARSAT-3K. USAF Sat Cat: 40272 . COSPAR: 2014-062B. Apogee: 35,793 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0600 deg. Period: 1,436.09 min. Argentina's first domestic geosynchronous communications satellite. Used a domestic satellite bus with 24 Ku-band transponder. Stationed in geosynchronous orbit at 72 deg west..

• DirecTV-14 - . Payload: SSL-MDA 1300. Mass: 6,300 kg (13,800 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 40333 . COSPAR: 2014-078B. Apogee: 35,789 km (22,238 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.0100 deg. Period: 1,436.11 min. Direct broadcast satellite. Stationed in geosynchronous orbit at 76 deg west..

• GSAT-16 - . Mass: 3,180 kg (7,010 lb). Nation: India. Class: Communications. Type: Communications satellite. Spacecraft: I-3K. USAF Sat Cat: 40332 . COSPAR: 2014-078A. Apogee: 35,802 km (22,246 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.11 deg. Period: 1,436.12 min. Communications satellite for the Indian Space Research Organization with Ku and C band payloads. Stationed in geosynchronous orbit at 55 deg east..

• Thor 7 - . Mass: 4,800 kg (10,500 lb). Nation: Norway. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 40613 . COSPAR: 2015-022A. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0100 deg. Period: 1,436.09 min. Provided broadcast services for Norway's Telenor, including a Ka-band payload dedicated to maritime and Antarctic communications. Stationed in geosynchronous orbit at 11.7 deg west..

• Sicral 2 - . Mass: 3,000 kg (6,600 lb). Nation: France. Class: Communications. Type: Communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 40614 . COSPAR: 2015-022B. Apogee: 35,800 km (22,200 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Secure communications for the Italian and French armed forces. Stationed in geosynchronous orbit..

• DirecTV-15 - . Mass: 6,205 kg (13,679 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 40663 . COSPAR: 2015-026A. Apogee: 35,790 km (22,230 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.0100 deg. Period: 1,436.13 min. Direct broadcast satellite for DirecTV. Geostationary, at 78.8W..

• SKYM-1 - . Mass: 3,182 kg (7,015 lb). Nation: Mexico. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 40664 . COSPAR: 2015-026B. Apogee: 35,794 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0100 deg. Period: 1,436.11 min. Television broadcast satellite for Sky Mexico, a joint venture of DirecTV and Mexico's Televisa. Geostationary, at 66.8W..

• Meteosat 11 - . Payload: MSG 4. Mass: 2,000 kg (4,400 lb). Nation: Europe. Class: Earth. Type: Weather satellite. Spacecraft: MSG. USAF Sat Cat: 40732 . COSPAR: 2015-034A. Apogee: 35,793 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 2.94 deg. Period: 1,436.11 min. Meteosat Second Generation (MSG) 4 ; redesignated Meteosat 11 once in operation with EUMETSAT, the European Meteorological Satellite Organization. Geosynchronous orbit stationed at 03.5W.

• Star One C4 - . Payload: STARONE C4. Mass: 5,635 kg (12,423 lb). Nation: Brazil. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 40733 . COSPAR: 2015-034B. Apogee: 35,792 km (22,240 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.0500 deg. Period: 1,436.11 min. Direct broadcast television satellite for the Brazilian operator Embratel Star One. Geosynchronous orbit stationed at 70W.

• Intelsat IS-34 - . Mass: 3,300 kg (7,200 lb). Nation: International. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 40874 . COSPAR: 2015-039A. Apogee: 35,790 km (22,230 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0200 deg. Period: 1,436.10 min. Communications satellite launched to replace Intelsat 805 and Galaxy 11 with C and Ku-band payloads. The Ku-band capacity will be partly used by Hispasat. Geosynchronous orbit stationed at 51.5W.

• Eutelsat 8 West B - . Payload: Spacebus 4000C4. Mass: 5,782 kg (12,747 lb). Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 40875 . COSPAR: 2015-039B. Apogee: 35,800 km (22,200 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.0600 deg. Period: 1,436.10 min. Eutelsat communications satellite with a Ku/C band payload. Geosynchronous orbit stationed at 01.7E.

• Sky Muster - . Mass: 6,300 kg (13,800 lb). Nation: Australia. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 40940 . COSPAR: 2015-054A. Apogee: 35,799 km (22,244 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.0300 deg. Period: 1,436.10 min.

  NBN 1 communications satellite, with a Ka-band payload for the Australian NBN Corporation, a government-owned company running the national broadband network. Purpose was to provide access to high speed broadband to every household and business in the country.

• ARSAT-2 - . Mass: 2,900 kg (6,300 lb). Nation: Argentina. Class: Communications. Type: Communications satellite. Spacecraft: ARSAT-3K. USAF Sat Cat: 40941 . COSPAR: 2015-054B. Apogee: 35,792 km (22,240 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.0600 deg. Period: 1,436.10 min. Argentinan indigenous communications satellite. 26 Ku-band and 10 C-band transponders..

• Badr 7 - . Payload: GSAT 15. Mass: 6,100 kg (13,400 lb). Nation: India. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 41028 . COSPAR: 2015-065A. Apogee: 35,764 km (22,222 mi). Perigee: 35,643 km (22,147 mi). Inclination: 0.10 deg. Period: 1,431.85 min. Also known as Arabsat-6B; communications satellite with Ku and Ka-band communications payloads..

• GSAT-15 - . Mass: 3,164 kg (6,975 lb). Nation: Arab States. Class: Communications. Type: Communications satellite. Spacecraft: I-3K. USAF Sat Cat: 41029 . COSPAR: 2015-065B. Apogee: 35,731 km (22,202 mi). Perigee: 254 km (157 mi). Inclination: 3.96 deg. Period: 631.04 min. Communications satellite with a Ku-band payload for Indian domestic television broadcasting as well as a GAGAN navigation payload..

• Intelsat IS-29e - . Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: HS 702. USAF Sat Cat: 41308 . COSPAR: 2016-004A. Apogee: 35,525 km (22,074 mi). Perigee: 280 km (170 mi). Inclination: 0.60 deg.

  Intelsat communications satellite in a low-inclination geotransfer orbit; carried C, Ku and Ka-band communications payload and was the first of Intelsat's new broadband high-throughput 'Epic-NG' series, built by Boeing using the BSS-702MP bus. Launch mass was 6552 kg.

• Eutelsat 65 West A - . Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 41382 . COSPAR: 2016-014A. Apogee: 35,759 km (22,219 mi). Perigee: 35,729 km (22,200 mi). Inclination: 0.00 deg.

  Ariane 5 vehicle L582, mission VA229 to a low inclination geotransfer with Eutelsat do Brasil's 65 West A payload, a Loral 1300 satellite. By Mar 14, 65 West A was in a 35729 x 35759 km x 0.0 deg near-GEO over the Atlantic. Placed in geosynchronous orbit at 44 deg W.

• Echostar 18 - . Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 41592 . COSPAR: 2016-039B. Apogee: 35,796 km (22,242 mi). Perigee: 33,289 km (20,684 mi). Inclination: 0.10 deg.

• BRISat - . Nation: Europe. Class: Communications. Type: Communications satellite. USAF Sat Cat: 41591 . COSPAR: 2016-039A. Apogee: 35,702 km (22,184 mi). Perigee: 32,931 km (20,462 mi). Inclination: 0.00 deg. Ariane 5 vehicle L584 put two communications satellites in geotransfer orbit. BRISat was dedicated to banking services for the Indonesian bank PT Bank Rakyat Indonesia (Persero) Tbk. of Jakarta..

• Intelsat IS-33e - . Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: HS 702. USAF Sat Cat: 41748 . COSPAR: 2016-053B. Apogee: 35,804 km (22,247 mi). Perigee: 15,756 km (9,790 mi). Inclination: 0.60 deg.

  Second Epic high throughput broadband satellite, a Boeing BSS-702MP model. Suffered suffered a failure of its main Leros apogee thruster in geotransfer orbit. Orbit raising was delayed until late September; by Oct 18 the satellite was in a 31428 x 35927 km x 0.1 deg orbit.

• Intelsat IS-36 - . Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 41747 . COSPAR: 2016-053A. Apogee: 35,759 km (22,219 mi). Perigee: 35,721 km (22,195 mi). Inclination: 0.10 deg. Small Ku/C-band satellite for video distribution..

• Sky Muster II - . Nation: Australia. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 41794 . COSPAR: 2016-060B. Apogee: 35,806 km (22,248 mi). Perigee: 35,292 km (21,929 mi). Inclination: 0.10 deg. Communications satellite for the Australian NBN broadcaster.

• GSAT-18 - . Nation: India. Class: Communications. Type: Communications satellite. Spacecraft: I-3K. USAF Sat Cat: 41793 . COSPAR: 2016-060A. Apogee: 35,831 km (22,264 mi). Perigee: 24,135 km (14,996 mi). Inclination: 0.50 deg. Ariane vehicle L585 mission VA231, placed two communications sats in geotransfer orbit. GSAT-18 was for the Indian Space Research Organization..

• GalileoSat-15 - . Payload: Galileo 15 (267). Nation: Europe. Class: Navigation. Type: Navigation satellite. Spacecraft: Galileo Navsat. USAF Sat Cat: 41859 . COSPAR: 2016-069A. Apogee: 22,906 km (14,233 mi). Perigee: 22,879 km (14,216 mi). Inclination: 54.60 deg.

  Four more European navigation satellites in the Galileo system were launched. An Ariane 5ES rocket was used; the restartable EPS upper stage placed the satellites (FM07, FM12, FM13 and FM14, redesignated GalileoSat 15 to 18 after launch) in orbit. The 5ES model was previously used for ATV cargo ship launches.

• GalileoSat-16 - . Payload: Galileo 16 (26C). Nation: Europe. Class: Navigation. Type: Navigation satellite. Spacecraft: Galileo Navsat. USAF Sat Cat: 41860 . COSPAR: 2016-069B. Apogee: 22,926 km (14,245 mi). Perigee: 22,890 km (14,220 mi). Inclination: 54.60 deg.

• GalileoSat-17 - . Payload: Galileo 17 (26D). Nation: Europe. Class: Navigation. Type: Navigation satellite. Spacecraft: Galileo Navsat. USAF Sat Cat: 41861 . COSPAR: 2016-069C. Apogee: 22,912 km (14,236 mi). Perigee: 22,901 km (14,229 mi). Inclination: 54.60 deg.

• GalileoSat-18 - . Payload: Galileo 18 (26E). Nation: Europe. Class: Navigation. Type: Navigation satellite. Spacecraft: Galileo Navsat. USAF Sat Cat: 41862 . COSPAR: 2016-069D. Apogee: 22,899 km (14,228 mi). Perigee: 22,898 km (14,228 mi). Inclination: 54.50 deg.

• JCSAT 15 - . Nation: Japan. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 41903 . COSPAR: 2016-082A. Apogee: 35,774 km (22,228 mi). Perigee: 35,721 km (22,195 mi). Inclination: 0.10 deg.

  Placed in geosynchronous orbit at 135 deg E. Ariane vehicle L587, mission VA234, placed two comm satellites in orbit. JCSAT 15, for Sky Perfect JSAT of Japan, was to become JCSAT-110A operational at 110E to replace JCSAT-110R. Loral 1300 class satellites built in MDA/Loral's Palo Alto factory.

• Star One D1 - . Nation: Brazil. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 41904 . COSPAR: 2016-082B. Apogee: 35,777 km (22,230 mi). Perigee: 35,741 km (22,208 mi). Inclination: 0.10 deg. Loral 1300 class satellites built in MDA/Loral's Palo Alto factory for Embratel Star One of Brazil, to replace Brasilsat B4. Placed in geosynchronous orbit at 86 deg W..

• SkyBrasil-1 - . Payload: Intelsat 32E. Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 41945 . COSPAR: 2017-007B. Apogee: 35,785 km (22,235 mi). Perigee: 35,662 km (22,159 mi). Inclination: 0.10 deg. See Sky-Brasil 1 (Intelsat 32e). Communications satellite for AT&T/DirectTV Latin America and Intelsat (which called the satellite Intelsat-32e)..

• Telkom-3S - . Nation: Indonesia. Class: Communications. Type: Communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 41944 . COSPAR: 2017-007A. Apogee: 35,810 km (22,250 mi). Perigee: 35,641 km (22,146 mi). Inclination: 0.00 deg. See Telkom 3S. The VA235 flight placed two communications satellites in geotransfer orbit. Telkom-3S was for the Indonesian operator Telkom..

• Koreasat 7 - . Nation: Korea South. USAF Sat Cat: 42691 . COSPAR: 2017-023A. Apogee: 35,794 km (22,241 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0200 deg. Period: 1,436.12 min. See Koreasat 7. ..

• SGDC - . Nation: Brazil. USAF Sat Cat: 42692 . COSPAR: 2017-023B. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0500 deg. Period: 1,436.09 min. See SGDC 1. ..

• ViaSat-2 - . Nation: USA. USAF Sat Cat: 42740 . COSPAR: 2017-029A. Apogee: 35,788 km (22,237 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.0200 deg. Period: 1,436.12 min. See ViaSat 2. ..

• EUTELSAT 172B - . Nation: Europe. USAF Sat Cat: 42741 . COSPAR: 2017-029B. Apogee: 35,800 km (22,200 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.0100 deg. Period: 1,436.10 min. See Eutelsat 172B. ..

• Hellas Sat 3-Inmarsat S EAN - . Payload: Hellas Sat 3; HELLAS-SAT 3. Nation: Europe. USAF Sat Cat: 42814 . COSPAR: 2017-040A. Apogee: 35,803 km (22,246 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.0700 deg. Period: 1,436.11 min. See HellasSat 3 / Inmarsat-S-EAN (EuropaSat). ..

• GSAT-17 - . Nation: India. USAF Sat Cat: 42815 . COSPAR: 2017-040B. Apogee: 35,810 km (22,250 mi). Perigee: 35,764 km (22,222 mi). Inclination: 0.0100 deg. Period: 1,436.12 min. See GSat 17. ..

• Intelsat IS-37e - . Nation: USA. USAF Sat Cat: 42950 . COSPAR: 2017-059A. Apogee: 35,796 km (22,242 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0200 deg. Period: 1,436.12 min. See Intelsat 37e. ..

• BSAT-4a - . Nation: Japan. USAF Sat Cat: 42951 . COSPAR: 2017-059B. Apogee: 35,802 km (22,246 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.0400 deg. Period: 1,436.08 min. See BSat 4a. ..

• GalileoSat-19 - . Payload: Galileo FOC FM15; GALILEO 19 (2C5). Nation: Europe. USAF Sat Cat: 43055 . COSPAR: 2017-079A. Apogee: 23,226 km (14,431 mi). Perigee: 23,218 km (14,426 mi). Inclination: 56.66 deg. Period: 844.71 min. See Galileo 19 (Galileo-FOC FM15, Nicole). ..

• GalileoSat-20 - . Payload: Galileo FOC FM16; GALILEO 20 (2C6). Nation: Europe. USAF Sat Cat: 43056 . COSPAR: 2017-079B. Apogee: 23,232 km (14,435 mi). Perigee: 23,213 km (14,423 mi). Inclination: 56.67 deg. Period: 844.70 min. See Galileo 20 (Galileo-FOC FM16, Zofia). .. Additional Details: here....

• GalileoSat-21 - . Payload: Galileo FOC FM17; GALILEO 21 (2C7). Nation: Europe. USAF Sat Cat: 43057 . COSPAR: 2017-079C. Apogee: 23,231 km (14,435 mi). Perigee: 23,213 km (14,423 mi). Inclination: 56.67 deg. Period: 844.71 min. See Galileo 21 (Galileo-FOC FM17, Alexandre). .. Additional Details: here....

• GalileoSat-22 - . Payload: Galileo FOC FM18; GALILEO 22 (2C8). Nation: Europe. USAF Sat Cat: 43058 . COSPAR: 2017-079D. Apogee: 23,233 km (14,436 mi). Perigee: 23,212 km (14,423 mi). Inclination: 56.66 deg. Period: 844.70 min. See Galileo 22 (Galileo-FOC FM18, Irina). .. Additional Details: here....

• Al Yah 3 - . Nation: UAE. USAF Sat Cat: 43174 . COSPAR: 2018-012A. Apogee: 35,795 km (22,241 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0100 deg. Period: 1,436.14 min. See Al Yah 3. ..

• SES-14 - . Nation: SES. USAF Sat Cat: 43175 . COSPAR: 2018-012B. Apogee: 35,789 km (22,238 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.0200 deg. Period: 1,436.14 min. See SES 14/GOLD. ..

• Kirameki 1 - . Payload: Superbird 8/DSN 1; SUPERBIRD 8. Nation: Japan. USAF Sat Cat: 43271 . COSPAR: 2018-033A. Apogee: 35,789 km (22,238 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0500 deg. Period: 1,436.07 min. See DSN 1/Superbird 8 (Kirameki 1/Superbird B3). ..

• Hylas 4 - . Payload: BSAT-4a. Nation: UK. USAF Sat Cat: 43272 . COSPAR: 2018-033B. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0600 deg. Period: 1,436.10 min. See HYLAS 4. ..

• GalileoSat-23 - . Payload: Galileo FOC FM19; GALILEO 25 (2C1). Nation: Europe. USAF Sat Cat: 43564 . COSPAR: 2018-060A. Apogee: 23,241 km (14,441 mi). Perigee: 23,203 km (14,417 mi). Inclination: 56.47 deg. Period: 844.69 min. See Galileo 23 (Galileo-FOC FM19, Tara). ..

• GalileoSat-24 - . Payload: Galileo FOC FM20; GALILEO 26 (2C2). Nation: Europe. USAF Sat Cat: 43565 . COSPAR: 2018-060B. Apogee: 23,240 km (14,440 mi). Perigee: 23,203 km (14,417 mi). Inclination: 56.47 deg. Period: 844.69 min. See Galileo 24 (Galileo-FOC FM20, Samuel). .. Additional Details: here....

• GalileoSat-25 - . Payload: Galileo FOC FM21; GALILEO 23 (2C9). Nation: Europe. USAF Sat Cat: 43566 . COSPAR: 2018-060C. Apogee: 23,239 km (14,440 mi). Perigee: 23,205 km (14,418 mi). Inclination: 56.47 deg. Period: 844.69 min. See Galileo 25 (Galileo-FOC FM21, Anna). .. Additional Details: here....

• GalileoSat-26 - . Payload: Galileo FOC FM22; GALILEO 24 (2C0). Nation: Europe. USAF Sat Cat: 43567 . COSPAR: 2018-060D. Apogee: 23,239 km (14,440 mi). Perigee: 23,204 km (14,418 mi). Inclination: 56.47 deg. Period: 844.69 min. See Galileo 26 (Galileo-FOC FM22, Ellen). .. Additional Details: here....

• Azerspace-2 - . Payload: Intelsat IS-38. Nation: Azerbaijan. USAF Sat Cat: 43632 . COSPAR: 2018-074A. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0200 deg. Period: 1,436.10 min. See Horizons 3e. ..

• Horizons 3e - . Nation: USA. USAF Sat Cat: 43633 . COSPAR: 2018-074B. Apogee: 35,791 km (22,239 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.0400 deg. Period: 1,436.19 min. See Horizons 3e. ..

• BepiColombo MPO - . Payload: Mercury Planetary Orbiter. Nation: Europe. USAF Sat Cat: 43653 . COSPAR: 2018-080A. See BepiColombo-MPO. ..

• Mio - . Payload: Mercury Magnetospheric Or. COSPAR: 2018-080C. See BepiColombo-MMO (Mio). ..

• Geo-Kompsat 2A - . Nation: Korea South. Type: Comms 1. USAF Sat Cat: 43823 . COSPAR: 2018-100A. Apogee: 35,746 km (22,211 mi). Perigee: 35,607 km (22,125 mi). Inclination: 0.0600 deg. Period: 1,430.50 min. See GEO-KOMPSAT 2A (GK 2A, Cheollian 2A). ..

• GSAT-11 - . Nation: India. Type: Comms 1. USAF Sat Cat: 43824 . COSPAR: 2018-100B. Apogee: 35,803 km (22,246 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.15 deg. Period: 1,436.08 min. See GSat 11. ..