Encyclopedia Astronautica
FS-1300



fs1300.jpg
FS-1300
American communications satellite bus. Operational, first launch 1989.06.05.

The 1300 was Space Systems/Loral's space-proven platform for a wide range of services, although its primary use was for geosynchronous communications satellites. From its first flight in 1989, it underwent constant evolutionary development to deliver greater power, communications capability, and longer useful life. Sales continued brisk well into the 21st Century.

Total satellite power was from 5 to 12 kW continuously throughout the life of the spacecraft. On-board transmitter power - exceeding 5,000 RF watts -- could accommodate as many as 70 active transponders. Launch masses ranged up to 5,500 kg and the spacecraft was equipped with a bipropellant propulsion system. The 1300S version provided up to 40 percent greater capacity than the 1300. Total satellite power ranged from 12 to 18 kW throughout the life of the spacecraft. On-board transmitter power - approaching 10,000 RF watts -- could accommodate as many as 90 active transponders. Launch masses up to 6,700 kilograms were possible and the spacecraft was equipped with an ion station-keeping engine to supplement the bipropellant propulsion system. Some FS 1300 series satellites were retired after 17 years of successful service, more than twice their design life. A 4 m diameter payload fairing was required.

Gross mass: 6,700 kg (14,700 lb).
First Launch: 1989.06.05.
Last Launch: 2011.10.19.
Number: 79 .

More... - Chronology...


Associated Countries
See also
  • Ariane 5 The Ariane 5 was a completely new design, unrelated to the earlier Ariane 1 to 4. It consisted of a single-engine Lox/LH2 core stage flanked by two solid rocket boosters. Preparatory work began in 1984. Full scale development began in 1988 and cost $ 8 billion. The design was sized for the Hermes manned spaceplane, later cancelled. This resulted in the booster being a bit too large for the main commercial payload, geosynchronous communications satellites. As a result, development of an uprated version capable of launching two such satellites at a time was funded in 2000. More...
  • Ariane First successful European commercial launch vehicle, developed from L3S Europa launch vehicle replacement design. Development of the Ariane 1 was authorised in July 1973, took eight years, and cost 2 billion 1986 Euros. More...
  • Atlas The Atlas rocket, originally developed as America's first ICBM, was the basis for most early American space exploration and was that country's most successful medium-lift commercial launch vehicle. It launched America's first astronaut into orbit; the first generations of spy satellites; the first lunar orbiters and landers; the first probes to Venus, Mars, Mercury, Jupiter, and Saturn; and was America's most successful commercial launcher of communications satellites. Its innovative stage-and-a-half and 'balloon tank' design provided the best dry-mass fraction of any launch vehicle ever built. It was retired in 2004 after 576 launches in a 47-year career. More...
  • Atlas V The Atlas V launch vehicle system was a completely new design that succeeded the earlier Atlas series. Atlas V vehicles were based on the 3.8-m (12.5-ft) diameter Common Core Booster (CCB) powered by a single Russian RD-180 engine. These could be clustered together, and complemented by a Centaur upper stage, and up to five solid rocket boosters, to achieve a wide range of performance. More...
  • CZ China's first ICBM, the DF-5, first flew in 1971. It was a two-stage storable-propellant rocket in the same class as the American Titan, the Russian R-36, or the European Ariane. The DF-5 spawned a long series of Long March ("Chang Zheng") CZ-2, CZ-3, and CZ-4 launch vehicles. These used cryogenic engines for upper stages and liquid-propellant strap-on motors to create a family of 12 Long-March rocket configurations capable of placing up to 9,200 kg into orbit. In 2000 China began development of a new generation of expendable launch vehicles using non-toxic, high-performance propellants with supposedly lower operating costs. However these encountered development delays, and it seemed the reliable Long March series of rockets would continue in operational use for nearly fifty years before being replaced. More...
  • H-2 Heavy lift Japanese indigenous launch vehicle. The original H-2 version was cancelled due to high costs and poor reliability and replaced by the substantially redesigned H-2A.

    3 stage vehicle consisted of 2 x H-II SRB + 1 x H-II stage 1 + 1 x H-II stage 2 More...

  • Proton The Proton launch vehicle has been the medium-lift workhorse of the Soviet and Russian space programs for over forty years. Although constantly criticized within Russia for its use of toxic and ecologically-damaging storable liquid propellants, it has out-lasted all challengers, and no replacement is in sight. More...
  • Zenit Zenit was to be a modular new generation medium Soviet launch vehicle, replacing the various ICBM-derived launch vehicles in use since the 1960's (Tsiklon and Soyuz). A version of the first stage was used as strap-ons for the cancelled Energia heavy booster. But it was built by Yuzhnoye in the Ukraine; when the Soviet Union broke up planned large-scale production for the Soviet military was abandoned (Angara development was begun as an indigenous alternative). Launch pads were completed only at Baikonur; those at Plesetsk were never finished and are planned to be completed as Angara pads. However the vehicle found new life as a commercial launch vehicle, launched from a sea platform by an American/Ukrainian consortium. More...

Associated Launch Vehicles
  • Atlas The Atlas rocket, originally developed as America's first ICBM, was the basis for most early American space exploration and was that country's most successful medium-lift commercial launch vehicle. It launched America's first astronaut into orbit; the first generations of spy satellites; the first lunar orbiters and landers; the first probes to Venus, Mars, Mercury, Jupiter, and Saturn; and was America's most successful commercial launcher of communications satellites. Its innovative stage-and-a-half and 'balloon tank' design provided the best dry-mass fraction of any launch vehicle ever built. It was retired in 2004 after 576 launches in a 47-year career. More...
  • Proton The Proton launch vehicle has been the medium-lift workhorse of the Soviet and Russian space programs for over forty years. Although constantly criticized within Russia for its use of toxic and ecologically-damaging storable liquid propellants, it has out-lasted all challengers, and no replacement is in sight. Development of the Proton began in 1962 as a two-stage vehicle that could be used to launch large military payloads or act as a ballistic missile with a 100 megaton nuclear warhead. The ICBM was cancelled in 1965, but development of a three-stage version for the crash program to send a Soviet man around the moon began in 1964. The hurried development caused severe reliability problems in early production. But these were eventually solved, and from the 1970's the Proton was used to launch all Russian space stations, medium- and geosynchronous orbit satellites, and lunar and planetary probes. More...
  • CZ Chinese orbital launch vehicle. China's first ICBM, the DF-5, first flew in 1971. It was a two-stage storable-propellant rocket in the same class as the American Titan, the Russian R-36, or the European Ariane. The DF-5 spawned a long series of Long March ("Chang Zheng") CZ-2, CZ-3, and CZ-4 launch vehicles. These used cryogenic engines for upper stages and liquid-propellant strap-on motors to create a family of 12 Long-March rocket configurations capable of placing up to 9,200 kg into orbit. In 2000 China began development of a new generation of expendable launch vehicles using non-toxic, high-performance propellants with supposedly lower operating costs. However these encountered development delays, and it seemed the reliable Long March series of rockets would continue in operational use for nearly fifty years before being replaced. More...
  • Ariane French orbital launch vehicle. First successful European commercial launch vehicle, developed from L3S Europa launch vehicle replacement design. Development of the Ariane 1 was authorised in July 1973, took eight years, and cost 2 billion 1986 Euros. More...
  • Zenit Zenit was to be a modular new generation medium Soviet launch vehicle, replacing the various ICBM-derived launch vehicles in use since the 1960's (Tsiklon and Soyuz). A version of the first stage was used as strap-ons for the cancelled Energia heavy booster. But it was built by Yuzhnoye in the Ukraine; when the Soviet Union broke up planned large-scale production for the Soviet military was abandoned (Angara development was begun as an indigenous alternative). Launch pads were completed only at Baikonur; those at Plesetsk were never finished and are planned to be completed as Angara pads. However the vehicle found new life as a commercial launch vehicle, launched from a sea platform by an American/Ukrainian consortium. More...
  • Ariane 44LP French orbital launch vehicle. Ariane 4 with 2 liquid rocket + 2 solid rocket strap-ons. More...
  • Ariane 44L French orbital launch vehicle. Ariane 4 with 4 liquid rocket strap-ons. More...
  • Ariane 42P French orbital launch vehicle. Ariane 4 with 2 solid rocket strap-ons. More...
  • Ariane 44P French orbital launch vehicle. Ariane 4 with 4 solid rocket strap-ons. More...
  • Atlas IIA American orbital launch vehicle. Atlas IIA was a commercial derivative of the Atlas II developed for the US Air Force. Higher performance RL10A-4 (or RL10A-4-1) engines replaced Atlas II's RL10A-3-3A engines. More...
  • Atlas IIAS American orbital launch vehicle. The Atlas II booster was 2.7-meters longer than the Atlas I and included uprated Rocketdyne MA-5A engines. The Atlas I vernier engines were replaced with a hydrazine roll control system. The Centaur stage was stretched 0.9-meters compared to the Centaur I stage. Fixed foam insulation replaced Atlas I's jettisonable insulation panels. Higher performance RL10A-4 or RL10A-4-1 engines replaced Atlas II's RL10A-3-3A. The Atlas IIAS model added four Thiokol Castor IVA solid rocket boosters (SRBs) to the core Atlas stage to augment thrust for the first two minutes of flight. More...
  • Proton-K/DM-2M This four stage version uses the Block DM-2M / 11S861-01 upper stage, which has its own self-contained guidance unit. This reduces payload but does not require the spacecraft's guidance system to provide steering commands to booster. Used for launches of Russian geosynchronous satellites from 1994 on. More...
  • H-II Japanese orbital launch vehicle. 3 stage vehicle consisted of 2 x H-II SRB boosters + core vehicle. More...
  • H-2 Heavy lift Japanese indigenous launch vehicle. The original H-2 version was cancelled due to high costs and poor reliability and replaced by the substantially redesigned H-2A. More...
  • CZ-3B Chinese orbital launch vehicle. The Long March 3B was the most powerful Long March launch vehicle. It could inject a 5,000 kg payload into geosynchronous transfer orbit. The CZ-3B was developed on the basis of the CZ-3A, but had enlarged propellant tanks, larger fairing, and four boosters strapped onto the core stage. The CZ-3B boosters were identical to those of the CZ-3A. More...
  • Ariane 5 French orbital launch vehicle. The Ariane 5 was a completely new design, unrelated to the earlier Ariane 1 to 4. It consisted of a single-engine Lox/LH2 core stage flanked by two solid rocket boosters. Preparatory work began in 1984. Full scale development began in 1988 and cost $ 8 billion. The design was sized for the Hermes manned spaceplane, later cancelled. This resulted in the booster being a bit too large for the main commercial payload, geosynchronous communications satellites. As a result, development of an uprated version capable of launching two such satellites at a time was funded in 2000. More...
  • Ariane 5G French orbital launch vehicle. Initial version of the Ariane 5, a bit too large for the main commercial geosynchronous communications satellite payloads. More...
  • Zenit-3SL Ukrainian orbital launch vehicle. From the beginning of the program a Zenit-3 version was proposed for geosynchronous launches using the N1/Proton Block D third stage. This had the potential of replacing the Proton in the role of geosynchronous launcher. It was considered for launch from Australia / Cape York in the 1980's. Finally a joint US-Norwegian-Ukraininan-Russian consortium was formed to launch the three stage commercial Zenit from the Odyssey floating launch platform in the Pacific Ocean. More...
  • Atlas IIIA American orbital launch vehicle. The Atlas IIIA was a development of the Atlas using Russian engines in place of the Rocketdyne MA-5 booster/sustainer group used on all previous models. It was the centerpiece of Lockheed Martin's strategy to remain a leader in the commercial launch services industry. However customers never materialized, and it was used for only two launches in 2002-2004 before being replaced by the Atlas V. More...
  • Atlas V American orbital launch vehicle. The Atlas V launch vehicle system was a completely new design that succeeded the earlier Atlas series. Atlas V vehicles were based on the 3.8-m (12.5-ft) diameter Common Core Booster (CCB) powered by a single Russian RD-180 engine. These could be clustered together, and complemented by a Centaur upper stage, and up to five solid rocket boosters, to achieve a wide range of performance. More...
  • Proton/Briz M Improved Proton orbital launch vehicle. Improvements in lower stages to reduce structural mass, increase thrust, and fully utilize propellants (reducing release of toxic chemicals in stage impact areas). Briz M storable propellant upper stage replaces Block D cyrogenic stage. More...
  • Proton/Briz M Improved Proton orbital launch vehicle. Improvements in lower stages to reduce structural mass, increase thrust, and fully utilize propellants (reducing release of toxic chemicals in stage impact areas). Briz M storable propellant upper stage replaces Block D cyrogenic stage. More...
  • Ariane 5ECA French orbital launch vehicle, first version of the evolved Ariane 5. The solid booster motors propellant load was increased by 2.43 tonnes and the case was welded, for a weight saving in dry mass of 1.9 tonnes. 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 tonne 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 geoscynchronous transfer orbit from 6 tonnes to 10.5 tonnes. More...
  • Atlas V 431 American orbital launch vehicle. Atlas V with 4-m diameter payload fairing, single engine Centaur upper stage, and three strap-on solid boosters. Payloads: 11,547 kg (25,458 lb) to sun synchronous orbit; 7,800 kg (17,196 lb) to geosynchronous transfer orbit. More...
  • Atlas V 421 American orbital launch vehicle. Atlas V with 4-m diameter payload fairing, single engine Centaur upper stage, and two strap-on solid boosters. Payloads: 10,168 kg (22,416 lb) to sun synchronous orbit; 7,000 kg (15,432 lb) to geosynchronous transfer orbit. More...

Associated Manufacturers and Agencies
Associated Programs
  • DirecTV DirecTV Incorporated began broadcast of satellite-to-home direct television services in mid-1994. Originally a subsidiary of Hughes Communications, the company faced as competitors the similar Primestar and USSB services, as well as older C-band satellite services and cable TV companies. By 2007 it had become the most successful American direct-broadcast television service. More...
  • Intelsat Intelsat operated the world's first commercial communications satellite. It has provided the scheduled transoceanic television and voice and data communications service ever since. More...
  • Panamsat Pan American Satellite, in Greenwich, Connecticut, USA, was founded in 1984 as part of Alpha Lyracom. It orbited a series of communications satellites providing television broadcast to the US and Latin American markets. In 1996 it merged with Hughes Galaxy. More...
  • Telstar Network of communications satellites, operated by AT&T Skynet, later Loral Skynet, Bedminster. More...
  • Tempo Geosynchronous communications satellite network More...

Bibliography
  • McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
  • McDowell, Jonathan, Jonathan's Space Report (Internet Newsletter), Harvard University, Weekly, 1989 to Present. Web Address when accessed: here.
  • Krebs, Gunter, Gunter's Space Page, University of Frankfurt, 1996. Web Address when accessed: here.
  • JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: here.
  • Vladimirov, A, "Tablitsa zapuskov RN 'Proton' i 'Proton K'", Novosti kosmonavtiki, 1998, Issue 10, page 25.
  • Lockheed Martin Coporation, Atlas Family Fact Sheets, September 1998.. Web Address when accessed: here.
  • McDowell, Jonathan, Launch Log, October 1998. Web Address when accessed: here.
  • National Space Science Center Planetary Page, As of 19 February 1999.. Web Address when accessed: here.
  • NASA/GSFC Orbital Information Group Website, Web Address when accessed: here.
  • Space-Launcher.com, Orbital Report News Agency. Web Address when accessed: here.

Associated Launch Sites
  • Cape Canaveral America's largest launch center, used for all manned launches. Today only six of the 40 launch complexes built here remain in use. Located at or near Cape Canaveral are the Kennedy Space Center on Merritt Island, used by NASA for Saturn V and Space Shuttle launches; Patrick AFB on Cape Canaveral itself, operated the US Department of Defense and handling most other launches; the commercial Spaceport Florida; the air-launched launch vehicle and missile Drop Zone off Mayport, Florida, located at 29.00 N 79.00 W, and an offshore submarine-launched ballistic missile launch area. All of these take advantage of the extensive down-range tracking facilities that once extended from the Cape, through the Caribbean, South Atlantic, and to South Africa and the Indian Ocean. More...
  • Baikonur Russia's largest cosmodrome, the only one used for manned launches and with facilities for the larger Proton, N1, and Energia launch vehicles. The spaceport ended up on foreign soil after the break-up of Soviet Union. The official designations NIIP-5 and GIK-5 are used in official Soviet histories. It was also universally referred to as Tyuratam by both Soviet military staff and engineers, and the US intelligence agencies. Since the dissolution of the Soviet Union the Russian Federation has insisted on continued use of the old Soviet 'public' name of Baikonur. In its Kazakh (Kazak) version this is rendered Baykonur. More...
  • Tanegashima Japan's main launch site for he larger N and H launch vehicles. In use for sounding rockets from 1967 and orbital launches from 1975. As of 2007 over 140 major launches had been made from the site. More...
  • Kourou After the agreement with newly independent Algeria for France to evacuate their launch sites in that country, a location near Biscarosse was selected for French missile testing. However since only launches westwards across the Bay of Biscay could be made from this site, it was unsuitable for France's Diamant orbital launch vehicle. After reviewing 14 potential sites, a location in the South American French colony of Guiana was selected. This would allow over-water launches to a tremendous range of possible orbital inclinations -- from -100.5 deg to 1.5 deg. Being near the equator, it would provide the maximum assist from the earth's rotation for launches into equatorial orbits. The decision was formalized in April 1964 and in July 1966 ELDO chose the site for future launches of the Europa II launch vehicle. More...
  • Xichang China's launch site for geosynchronous orbit launches. Xichang Satellite Launch Centre is situated in Xichang, Sichuan Province, south-western China. The launch pad is at 102.0 degrees East and 28.2 degrees North. The head office of the launch centre is located in Xichang City, about 65 kilometers away. Xichang Airport is 50 km away. A dedicated railway and highway lead directly to the launch site. More...
  • Kiritimati Kiritimati (Christmas Island) in the Pacific Ocean was originally selected by Von Braun in his Collier magazine series of the early 1950's as an ideal equatorial launch site. A half century later, Boeing Sea Launch used an offshore location for orbital launches. The launch platform was a seagoing converted Norwegian offshore oil rig. Between missions it was berthed in Long Beach, California. It was towed to a location off Kiritimati for launches of the Ukrainian Zenit-3 launch vehicle. More...
  • Cape Canaveral LC36A Atlas launch complex. Launch site built in 1960 for NASA's Atlas/Centaur development program, and used for launches of that launch vehicle until its retirement. More...
  • Cape Canaveral LC36B Atlas V, Atlas launch complex. Atlas Centaur launch pad, in service from 1964 until the retirement of the launch vehicle. More...
  • Cape Canaveral LC41 Titan, Atlas V launch complex. Complexes 40 and 41 were constructed as part of the Integrate-Transfer-Launch (ITL) Titan launch facility at the north end of Cape Canaveral in the early 1960s. Over the next three decades, the complexes supported a wide variety of military space missions involving Titan IIIC, Titan 34D and Titan IV. Complex 41 was deactivated at the end of 1977, then upgraded for the Titan IV program in the 1986-88 period. In October 1999, Complex 41 was demolished with high explosives in order for a new pad for launch of the Atlas 5 rocket to be erected. By then it had been the starting point for 27 Titan flights. More...

FS-1300 Chronology


1989 June 5 - . 22:37 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L V31.
  • Superbird A - . Payload: Superbird A / DFS-Kopernikus 1. Mass: 2,489 kg (5,487 lb). Nation: Japan. Agency: SCC. Program: Superbird. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. Completed Operations Date: 1991-02-01 . USAF Sat Cat: 20040 . COSPAR: 1989-041A. Apogee: 35,944 km (22,334 mi). Perigee: 35,931 km (22,326 mi). Inclination: 2.5000 deg. Period: 1,443.80 min. Japanese domestic business communications; 158 deg E. Positioned in geosynchronous orbit at 158 deg E in 1989-1990 As of 6 September 2001 located at 41.59 deg E drifting at 1.921 deg W per day. As of 2007 Mar 11 located at 166.35W drifting at 1.878W degrees per day.

1990 February 22 - . 23:17 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L V36. FAILURE: Exploded 100 seconds after liftoff due to water line blockage. This was caused by a piece of cloth found in the first stage Viking engine water cooling system.. Failed Stage: 1.
  • Superbird B - . Nation: Japan. Agency: SCC. Program: Superbird. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. Decay Date: 1990-02-23 . COSPAR: F900222A. Apogee: 9.00 km (5.50 mi). Summary: Launched with BS-2X. Targeted for Geosynch orbit..

1992 February 26 - . 23:58 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L V49.
  • Superbird B1 - . Mass: 2,560 kg (5,640 lb). Nation: Japan. Agency: SCC. Program: Superbird. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 21893 . COSPAR: 1992-010A. Apogee: 36,206 km (22,497 mi). Perigee: 36,057 km (22,404 mi). Inclination: 0.9000 deg. Period: 1,453.80 min. Stationed at 162 deg E. Domestic communications. Launching organization Arianespace. Launch time 2358 GMT. Positioned in geosynchronous orbit at 162 deg E in 1992-1999 As of 4 September 2001 located at 19.90 deg W drifting at 4.382 deg W per day. As of 2007 Mar 9 located at 164.51E drifting at 4.378W degrees per day.

1992 December 1 - . 22:48 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 42P. LV Configuration: Ariane 42P+ V55.
  • Superbird A1 - . Mass: 2,780 kg (6,120 lb). Nation: Japan. Agency: SCC. Program: Superbird. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 22253 . COSPAR: 1992-084A. Apogee: 35,800 km (22,200 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Stationed at 158 deg E. Domestic communications. Launching states: Japan and France. Launch time 2248 GMT. Positioned in geosynchronous orbit at 158 deg E in 1993-1999 As of 31 August 2001 located at 157.95 deg E drifting at 0.011 deg W per day. As of 2007 Mar 9 located at 158.03E drifting at 0.006W degrees per day.

1993 October 22 - . 06:46 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP+ V60.
  • Intelsat 701 - . Payload: Intelsat 7 F 1. Mass: 3,650 kg (8,040 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 22871 . COSPAR: 1993-066A. Apogee: 35,802 km (22,246 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. International communications. The Intelsat 7 and 7A series were nearly identical except for an increase in the number of Ku-band transponders in the 7A series. Spacecraft: 3-axis stabilised. Hydrazine propulsion system. Two large solar panels with 1-axis articulation provide 3900W BOL. Payload: 7: 26 C-Band and 10 Ku-Band transponders.18,000 telephone calls and 3 colour TV broadcasts simultaneously. Or up to 90,000 telephone circuits using digital circuit multiplication equipment (DCME).7A: 26 C-Band and 14 Ku-Band transponders.22,500 telephone calls and 3 colour TV broadcasts simultaneously. Or up to 112,500 telephone circuits using DCME. Three independently steerable, high-powered, Ku-band spot beams. Independently steerable C-band spot beam coverage. Positioned in geosynchronous orbit at 121 deg E in 1993; 174 deg E in 1994-1997; 180 deg W in 1997-1999 As of 6 September 2001 located at 179.91 deg W drifting at 0.004 deg W per day. As of 2007 Mar 9 located at 179.97W drifting at 0.001E degrees per day.

1994 June 17 - . 07:07 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP+ V64.
  • Intelsat 702 - . Mass: 3,695 kg (8,146 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23124 . COSPAR: 1994-034A. Apogee: 35,795 km (22,241 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0200 deg. Period: 1,436.07 min. Stationed at 1.03 deg W. Positioned in geosynchronous orbit at 38 deg W in 1994; 1 deg W in 1994-1996; 177 deg E in 1996-1999 As of 5 September 2001 located at 175.99 deg E drifting at 0.001 deg E per day. As of 2007 Mar 9 located at 54.82E drifting at 0.001E degrees per day.

1994 October 6 - . 06:35 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas IIAS. LV Configuration: Atlas IIAS AC-111 / Centaur II 8202.
  • Intelsat 703 - . Payload: NSS 703. Mass: 3,656 kg (8,060 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23305 . COSPAR: 1994-064A. Apogee: 35,792 km (22,240 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0400 deg. Period: 1,436.07 min. 38 C-band and 20 Ku-band transponders. Initially positioned in geosynchronous orbit at 177 deg E in 1994-1996. Then reassigned to Intelsat subsidiary New Skies, redesignated NSS 703, and moved to 57 deg E after 1996. At the crossroads of three continents, NSS-703 provided cross-connectivity for Europe, Africa and Asia. NSS-703 was used for video contribution from Europe to India and Africa, and was capable of bringing signals from London to India and Australia in one hop. NSS-703's coverage included a global beam, and two C-band hemispheric beams, which covered Africa and the triangle from Eastern Iran to Japan and Australia, including all of India and China. Three steerable Ku-band spot beams targeted Europe and Iran, Central Asia and Afghanistan-Pakistan-North India. Expected end of life March 2009. As of 2007 Mar 9 located at 56.96E drifting at 0.001E degrees per day.

1995 January 10 - . 06:18 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas IIAS. LV Configuration: Atlas IIAS AC-113 / Centaur II 8203.
  • Intelsat 704 - . Mass: 3,656 kg (8,060 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23461 . COSPAR: 1995-001A. Apogee: 36,113 km (22,439 mi). Perigee: 36,075 km (22,415 mi). Inclination: 2.2000 deg. Period: 1,451.80 min. Stationed at 66.0 deg E. Launch vehicle put payload into supersynchronous earth orbit with MRS trajectory option. Positioned in geosynchronous orbit at 66 deg E in 1995-1999 As of 29 August 2001 located at 66.03 deg E drifting at 0.005 deg W per day. As of 2007 Mar 10 located at 66.03E drifting at 0.002W degrees per day.

1995 March 22 - . 06:18 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas IIAS. LV Configuration: Atlas IIAS AC-115.
  • Intelsat 705 - . Mass: 3,669 kg (8,088 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23528 . COSPAR: 1995-013A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Stationed at 50.1 deg W. Launch vehicle put payload into supersynchronous earth orbit with MRS trajectory option. Positioned in geosynchronous orbit at 50 deg W in 1995-1996; 18 deg W in 1996-1999 As of 5 September 2001 located at 17.97 deg W drifting at 0.006 deg W per day. As of 2007 Mar 11 located at 50.01W drifting at 0.007W degrees per day.

1995 May 17 - . 06:34 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP-3 V73.
  • Intelsat 706 - . Mass: 4,180 kg (9,210 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23571 . COSPAR: 1995-023A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Stationed at 53.1 deg W. Positioned in geosynchronous orbit at 53 deg W in 1995-1999 As of 4 September 2001 located at 52.93 deg W drifting at 0.005 deg W per day. As of 2007 Mar 4 located at 50.24E drifting at 0.003E degrees per day..

1995 August 29 - . 06:41 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44P. LV Configuration: Ariane 44P-3 V77.
  • N-Star a - . Mass: 3,100 kg (6,800 lb). Nation: Japan. Agency: NTT. Program: N-STAR. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23651 . COSPAR: 1995-044A. Apogee: 35,791 km (22,239 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Stationed at 131.9 deg E. Positioned in geosynchronous orbit at 132 deg E in 1995-1999 As of 1 September 2001 located at 131.99 deg E drifting at 0.017 deg W per day. As of 2007 Mar 11 located at 25.96E drifting at 4.123W degrees per day..

1996 February 5 - . 07:19 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44P. LV Configuration: Ariane 44P-3 V83.
  • N-STAR b - . Mass: 3,400 kg (7,400 lb). Nation: Japan. Agency: NTT. Program: N-STAR. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23781 . COSPAR: 1996-007A. Apogee: 35,801 km (22,245 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.1000 deg. Period: 1,436.20 min. Summary: Geostationary at 128.9E. Positioned in geosynchronous orbit at 136 deg E in 1996-1999 As of 1 September 2001 located at 136.01 deg E drifting at 0.012 deg W per day. As of 2007 Mar 9 located at 136.04E drifting at 0.012W degrees per day..

1996 February 14 - . 19:01 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: Chang Zheng 3B CZ3B-1 (40). FAILURE: Guidance failure resulted in launch vehicle crashing 22 seconds after launch, killing or injuring 59 people.. Failed Stage: G.
  • Intelsat 708 - . Nation: International. Agency: PRC. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. COSPAR: F960214A. First attempted launch of a new version in the Long March family. Began to experience an anomaly in attitude about 2 seconds after launch, pitching down and yawing to the right. It augured in nose down at T+22 seconds and exploded violently, utterly destroying the launcher and its payload. The Chief-Designer of the launch vehicle organised an analysis team on the same day of the accident. Interpretation and analysis of the telemetered data indicated that the crash was caused by a change in the inertial reference. The explosion killed six and injured 57. Two of the killed were senior engineers with CASC.

1996 March 14 - . 07:11 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP-3 V84.
  • Intelsat 707 - . Mass: 4,175 kg (9,204 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23816 . COSPAR: 1996-015A. Apogee: 35,798 km (22,243 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. GEO. 26 C-band, 14 K-band transponders. Geostationary at 0.9W. Positioned in geosynchronous orbit at 1 deg W in 1996-1999 As of 5 September 2001 located at 0.97 deg W drifting at 0.001 deg E per day. As of 2007 Mar 10 located at 53.03W drifting at 0.007W degrees per day.

1996 June 15 - . 06:55 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44P. LV Configuration: Ariane 44P-3 V87.
  • Intelsat 709 - . Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23915 . COSPAR: 1996-035A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: 36 transponders Geostationary at 50.0W. Positioned in geosynchronous orbit at 50 deg W in 1996-1999 As of 4 September 2001 located at 49.96 deg W drifting at 0.015 deg W per day. As of 2007 Mar 11 located at 85.17E drifting at 0.004W degrees per day..

1997 March 8 - . 06:01 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas IIA. LV Configuration: Atlas IIA AC-128.
  • Tempo 2 - . Nation: USA. Agency: TCI. Manufacturer: Palo Alto. Program: Tempo. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 24748 . COSPAR: 1997-011A. Apogee: 35,792 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Geosynchronous. Stationed over 118.7W Launch vehicle put payload into subsynchronous earth orbit with MRS trajectory option. Positioned in geosynchronous orbit at 119 deg W in 1997-1999 As of 5 September 2001 located at 118.82 deg W drifting at 0.001 deg W per day. As of 2007 Mar 10 located at 42.64E drifting at 4.479W degrees per day.

1997 May 24 - . 17:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM4) 380-02.
  • Telstar 5 - . Nation: USA. Agency: Skynet. Program: Telstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 24812 . COSPAR: 1997-026A. Apogee: 35,794 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Geosynchronous. Stationed over 97.0W Positioned in geosynchronous orbit at 97 deg W in 1997-1999 As of 5 September 2001 located at 96.99 deg W drifting at 0.006 deg W per day. As of 2007 Mar 9 located at 97.04W drifting at 0.005W degrees per day..

1997 August 8 - . 06:46 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44P. LV Configuration: Ariane 44P-3 V98.
  • Panamsat 6 - . Payload: PAS 6. Nation: USA. Agency: Panamsat. Manufacturer: Palo Alto. Program: Panamsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 24891 . COSPAR: 1997-040A. Apogee: 35,796 km (22,242 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Positioned in geosynchronous orbit at 43 deg W in 1997-2002. As of 2004 Oct 17 located at 96.68W drifting at 1.977W degrees per day..

1997 August 19 - . 17:50 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: Chang Zheng 3B CZ3B-2 (46).
  • Agila 2 - . Payload: Mabuhay. Nation: Philippines. Agency: MPSC. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 24901 . COSPAR: 1997-042A. Apogee: 35,803 km (22,246 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.0000 deg. Period: 1,436.20 min. Summary: Geosynchronous. Stationed over 146.0E Positioned in geosynchronous orbit at 146 deg E in 1997-1999 As of 5 September 2001 located at 145.99 deg E drifting at 0.009 deg W per day. As of 2007 Mar 11 located at 145.98E drifting at 0.017W degrees per day..

1997 October 16 - . 19:13 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: Chang Zheng 3B CZ3B-3 (48).
  • Apstar 2R - . Nation: China. Agency: APT. Manufacturer: Palo Alto. Program: Apstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 25010 . COSPAR: 1997-062A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Geosynchronous. Stationed over 76.5E Positioned in geosynchronous orbit at 76 deg E in 1997-1999 As of 5 September 2001 located at 76.48 deg E drifting at 0.001 deg W per day. As of 2007 Mar 11 located at 76.46E drifting at 0.002W degrees per day..

1998 September 16 - . 06:31 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP-3 V110.
  • Panamsat 7 - . Payload: PAS 7. Nation: USA. Agency: Panamsat. Manufacturer: Palo Alto. Program: Panamsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 25473 . COSPAR: 1998-052A. Apogee: 35,798 km (22,243 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Geostationary at 68.7 degrees E. Positioned in geosynchronous orbit at 68 deg E in 1998-1999 As of 6 September 2001 located at 68.68 deg E drifting at 0.012 deg W per day. As of 2007 Mar 10 located at 68.67E drifting at 0.001W degrees per day..

1998 November 4 - . 05:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 395-02.
  • Panamsat 8 - . Payload: PAS 8. Nation: USA. Agency: Panamsat. Manufacturer: Palo Alto. Program: Panamsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 25522 . COSPAR: 1998-065A. Apogee: 35,810 km (22,250 mi). Perigee: 35,763 km (22,222 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. The Proton launch vehicles Block DM3 fourth stage put the Panamsat PAS 8 into a 6784 km x 35941 km x 17.3 degree transfer orbit. PAS 8 had 24 C-band and 24 Ku-band transponders and was to be located over the Pacific after its R-4D apogee engine manoeuvred the orbit to geostationary altitude and inclination. Geostationary at 166.1 degrees E. Positioned in geosynchronous orbit at 166 deg E in 1998-1999 As of 4 September 2001 located at 166.05 deg E drifting at 0.003 deg W per day. As of 2007 Mar 9 located at 165.96E drifting at 0.002E degrees per day.

1999 February 15 - . 05:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 396-01.
  • Telstar 6 - . Mass: 3,700 kg (8,100 lb). Nation: USA. Agency: Skynet. Manufacturer: Palo Alto. Program: Telstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 25626 . COSPAR: 1999-005A. Apogee: 35,796 km (22,242 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Loral Skynet's Telstar 6 had a mixed C and Ku band communications payload. The Block DM3 upper stage released Telstar 6 in a 6638 km x 35,756 km x 17.4 degree geosynchronous transfer orbit. After the first burn of its on-board R-4D engine on February 18, Telstar 6 was in a 15,037 km x 35,800 km x 7.9 deg transfer orbit heading for its final geosynchronous slot at 93 deg W Positioned in geosynchronous orbit at 93 deg W in 1999. As of 2 September 2001 located at 93.01 deg W drifting at 0.004 deg W per day. As of 2007 Mar 11 located at 93.03W drifting at 0.007W degrees per day.

1999 September 23 - . 06:02 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. Launch Pad: SLC36A. LV Family: Atlas. Launch Vehicle: Atlas IIAS. LV Configuration: Atlas IIAS AC-155.
  • Echostar 5 - . Nation: USA. Agency: PanAmSat. Manufacturer: Palo Alto. Program: Echostar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 25913 . COSPAR: 1999-050A. Apogee: 35,795 km (22,241 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. The Centaur second stage put Echostar 5 into a supersynchronous transfer orbit of 131 km x 45526 km x 26.6 degrees. The satellite's own engine put it into the final geosynchronous orbit. Echostar 5 was a Ku-band satellite, part of the Dish Network. Stationed at 110 deg W. Positioned in geosynchronous orbit at 110 deg W in 1999. As of 5 September 2001 located at 110.01 deg W drifting at 0.003 deg W per day. As of 2007 Mar 11 located at 128.86W drifting at 0.001E degrees per day.

1999 September 25 - . 06:29 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP-3 V121.
  • Telstar 7 - . Mass: 3,790 kg (8,350 lb). Nation: USA. Agency: Skynet. Manufacturer: Palo Alto. Program: Telstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 25922 . COSPAR: 1999-052A. Apogee: 35,794 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Telstar 7, owned by Loral Skynet, had 24 C-band and 24 Ku-band transponders. Dry mass was 1537 kg. After placement in final geosynchronous orbit it provided communications for North America from a position at 129 degrees East longitude. Sold to Intelsat in March 2004 and renamed IA-7. The satellite had a power failure on November 28, 2004 and was briefly declared lost. Intelsat recovered control of the satellite by December 4. As of 2007 Mar 9 located at 129.01W drifting at 0.007W degrees per day.

1999 October 19 - . 06:22 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP-3 V122.
  • Orion 2 - . Nation: USA. Agency: Arianespace. Manufacturer: Palo Alto. Program: Orion. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 25949 . COSPAR: 1999-059A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Satellite used for international communications; complement the Telstar satellites operated by Loral Skynet. Stationed at 15 deg W. Positioned in geosynchronous orbit at 15 deg W in 1999. As of 6 September 2001 located at 14.97 deg W drifting at 0.006 deg W per day. As of 2007 Mar 10 located at 14.99W drifting at 0.006W degrees per day.

1999 November 15 - . 07:29 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-II. LV Configuration: H-II H-II-8F. FAILURE: Failure during first stage burn.. Failed Stage: 1.
  • MTSAT - . Nation: Japan. Agency: NASDA. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. COSPAR: F991115A. Multi-functional Transportation Satellite intended to provide communications and air traffic control for the Japanese transportation ministry and a meteorological data for the Japanese Meteorological Agency. The spacecraft had a mass of 1223 kg dry and was a follow-on to the GMS (Himawari) weather satellite series.

2000 May 3 - . 07:07 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. Launch Pad: SLC36A. LV Family: Atlas. Launch Vehicle: Atlas IIA. LV Configuration: Atlas IIA AC-137.
  • GOES 11 - . Payload: GOES L. Mass: 2,217 kg (4,887 lb). Nation: USA. Agency: NOAA. Manufacturer: Palo Alto. Program: GOES. Class: Earth. Type: Weather satellite. Spacecraft: FS-1300. USAF Sat Cat: 26352 . COSPAR: 2000-022A. Apogee: 35,796 km (22,242 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.4000 deg. Period: 1,436.30 min. US civilian geostationary weather satellite in the Geostationary Operational Environmental Satellite series. It was the first GOES launch on the Atlas II launch vehicle (the Atlas I having been phased out). Built by SS/Loral, based on the FS-1300 bus. It was equipped with one solar panel array and a counter-boom with a solar sail. The satellite carried well as an imaging radiometer and an X-ray detector to monitor solar activity. Stationed at 106 deg W. Positioned in geosynchronous orbit at 104 deg W in 2000. As of 5 September 2001 located at 108.58 deg W drifting at 0.018 deg E per day. As of 2007 Mar 11 located at 135.52W drifting at 0.001E degrees per day.

2000 June 30 - . 22:08 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 400-01.
  • Sirius 1 - . Payload: CD Radio 1. Mass: 3,800 kg (8,300 lb). Nation: USA. Agency: Sirius. Manufacturer: Palo Alto. Program: Sirius. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 26390 . COSPAR: 2000-035A. Apogee: 47,107 km (29,270 mi). Perigee: 24,465 km (15,201 mi). Inclination: 63.4000 deg. Period: 1,436.10 min. Digital Audio Radio Satellite, used for transmission of S-band radio broadcasts direct to receivers in cars in the United States. Sirius 1 was inserted into an initial 6,166 x 47110 km x 63.4 deg transfer orbit by the Proton-K's Blok DM3 upper stage. The satellite's R4D liquid apogee engine made several burns to raise the orbit to 24,388 x 47,097 km x 63.3 deg by July 8. This elliptical, inclined 24 hour orbit had a 24 hour period, designed to keep the satellite between longitude 60W and 140W, with apogee over the northern hemisphere. Stationed at 66 deg W. Positioned in geosynchronous orbit at 66 deg W in 2000. As of 6 September 2001 located at 65.59 deg W drifting at 0.015 deg E per day. As of 2007 Mar 9 located at 65.37W drifting at 0.004E degrees per day.

2000 July 14 - . 05:21 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. Launch Pad: SLC36B. LV Family: Atlas. Launch Vehicle: Atlas IIAS. LV Configuration: Atlas IIAS AC-161.
  • Echostar 6 - . Mass: 3,700 kg (8,100 lb). Nation: USA. Agency: PanAmSat. Manufacturer: Palo Alto. Program: Echostar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 26402 . COSPAR: 2000-038A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Communications satellite, positioned in geosynchronous orbit at 149 deg W. By 5 September 2001 located at 119.07 deg W drifting at 0.002 deg W per day. As of 2007 Mar 10 located at 110.39W drifting at 0.006W degrees per day..

2000 September 5 - . 09:43 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 400-02.
  • Sirius 2 - . Mass: 3,800 kg (8,300 lb). Nation: USA. Agency: Sirius. Manufacturer: Palo Alto. Program: Sirius. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 26483 . COSPAR: 2000-051A. Apogee: 47,090 km (29,260 mi). Perigee: 24,480 km (15,210 mi). Inclination: 63.9000 deg. Period: 1,436.00 min. Sirius Radio's Sirius 2 was launched into a 144 x 168 km x 64.8 deg parking orbit. The Blok DM3 stage then made two burns to deliver Sirius 2 to an elliptical 6192 x 47057 km x 63.4 deg orbit. The was to provide digital radio broadcasts to mobile users in North America. Stationed at 64 deg W. As of 31 August 2001 located at 64.56 deg W drifting at 0.003 deg W per day. As of 2007 Mar 10 located at 67.77W drifting at 0.049E degrees per day.

2000 October 29 - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP-3 V134.
  • EuropeStar F1 - . Payload: Europe*Star FM1. Mass: 4,167 kg (9,186 lb). Nation: UK. Agency: EuropeSt. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 26590 . COSPAR: 2000-068A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. 100th Ariane 4 launch. Communications satellite, stationed at 45 deg E. Europeon.Star FM1 was a Loral FS-1300 model with a launch mass of 4167 kg and a dry mass of 1717 kg. The satellite had two cruciform solar arrays. The Ariane booster placed it into a geostationary transfer orbit. Positioned in geosynchronous orbit at 45 deg E in 2000. As of 4 September 2001 located at 44.95 deg E drifting at 0.011 deg E per day. As of 2007 Feb 23 located at 44.97E drifting at 0.001W degrees per day.

2000 November 30 - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 402-02.
  • Sirius CD Radio 3 - . Payload: CD Radio 3. Mass: 3,800 kg (8,300 lb). Nation: USA. Agency: Sirius. Manufacturer: Palo Alto. Program: Sirius. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 26626 . COSPAR: 2000-077A. Apogee: 47,084 km (29,256 mi). Perigee: 24,485 km (15,214 mi). Inclination: 64.2000 deg. Period: 1,436.00 min. Direct Radio Broadcasting satellite. Launch delayed from early October due to delays in delivery of engines. Stationed at 66 deg W. The third Sirius digital radio broadcast satellite was a Loral FS-1300 series vehicle and was placed in an initial elliptical 63 degree orbit by the Proton upper stage. Positioned in geosynchronous orbit at 66 deg W in 2000. As of 30 August 2001 located at 64.69 deg W drifting at 0.027 deg E per day. As of 2007 Mar 10 located at 65.64W drifting at 0.010E degrees per day.

2001 June 9 - . 06:45 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L-3 V141.
  • Intelsat 901 - . Mass: 4,725 kg (10,416 lb). Nation: International. Agency: Intelsat. Manufacturer: Palo Alto. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 26824 . COSPAR: 2001-024A. Apogee: 35,804 km (22,247 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Launch delayed from June 8. The first of the Intelsat 9 series provided telecommunications (Internet, video and telephone) services from a geosynchronous position at 18 deg W over the Atlantic Ocean. Intelsat 901 was an FS-1300HL, an improved version of the long-standing Space Systems/Loral (originally Aeronutronic Ford) FS-1300 platform. The satellite was to provide voice and video services to Europe and the Americas through 44 C-band and 12 Ku-band transponders. The satellite had C-band beams for the Atlantic region and a Ku-band spot beam for Europe, and an R-4D liquid apogee engine. Dry mass was 1972 kg and launch mass of 4723 kg. The International Telecommunications Satellite Organization (ITSO), beginning with its first satellite, Early Bird (1965-028A), had as of this date successfully launched 54 satellites, 19 of which were operational. As of 27 August 2001 located at 54.26 deg W drifting at 1.105 deg E per day. As of 2007 Mar 8 located at 18.01W drifting at 0.008W degrees per day.

2001 July 23 - . 07:23 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. Launch Pad: SLC36A. LV Family: Atlas. Launch Vehicle: Atlas IIA. LV Configuration: Atlas IIA AC-142.
  • GOES 12 - . Payload: GOES-M. Mass: 2,105 kg (4,640 lb). Nation: USA. Agency: NOAA. Manufacturer: Palo Alto. Program: GOES. Class: Earth. Type: Weather satellite. Spacecraft: FS-1300. USAF Sat Cat: 26871 . COSPAR: 2001-031A. Apogee: 35,813 km (22,253 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.0000 deg. Period: 1,436.30 min. Launch delayed from July 12, 15 and 22. The GOES-M weather satellite was placed by the Atlas AC-142 Centaur stage into a 164 x 505 km parking orbit and then a super synchronous transfer orbit of 274 x 42275 km x 20 deg. GOES-M was a Loral 1300-series satellite with a single solar array and a solar attitude control sail. Launch mass was 2279 kg and dry mass 1042 kg. The Geostationary Operational Environmental Satellites were developed by NASA-Goddard and were transferred to the NOAA weather agency when operational. In addition to the usual weather imager/sounder, GOES-M carried a new solar soft X-ray imager. Earlier GOES satellites carried simple X-ray collimator detectors, but the new SXI was a full-fledged grazing incidence telescope similar to the SXT on Japan's Yohkoh satellite. The GOES-M satellite was redesignated GOES 12 once in orbit.

    GOES 12 was a 980 kg, 973 W spacecraft that carried an IR imager, a "sounder", and an X-ray imager. The IR imager was a Cassegrain telescope covering five wavelength channels, 0.55-0.75, 3.80-4.00, 6.50-7.00, 10.20-11.20, and 11.50-12.50 microns. It provided images covering 3,000 km x 3,000 km every 41 seconds, by scanning the area in 16 square kilometer sections. The "sounder" provided vertical distribution of temperature, moisture and ozone, by passive monitoring in 18 depth-dependent wavelengths. (Long wave IR: 14.71, 14.37, 14.06, 13.64, 13.37, 12.66, and 12.02 microns. Medium wave IR: 11.03, 9.71, 7.43, 7.02, and 6.51 microns. Short wave IR: 4.57, 4.52, 4.45, 4.13, 3.98, and 3.74 microns. There was also another band at visible wavelength 0.7 microns, to provide pictures of cloud tops.) The sounder covered an area of 3,000 km x 3,000 km in about 42 minutes. Another instrument package named SEM (Space Environment Monitor) monitored the energetic electrons and protons in the magnetosphere and the X-rays from the Sun. The above three had been carried on the earlier GOES missions, but GOES 12 carried also an X-ray imager providing an X-ray (about 0.1-1.0 nm wavelength) picture of the solar disk. For some months, the spacecraft was to be on standby, to be activated and moved to a desired longitude. As of 5 September 2001 located at 89.93 deg W drifting at 0.001 deg W per day. As of 2007 Mar 11 located at 74.73W drifting at 0.014E degrees per day.


2001 August 30 - . 06:46 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L-3 V143.
  • Intelsat 902 - . Mass: 4,725 kg (10,416 lb). Nation: International. Agency: Intelsat. Manufacturer: Palo Alto. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 26900 . COSPAR: 2001-039A. Apogee: 35,801 km (22,245 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Launch delayed from August 24. The Intelsat 902 geosynchronous communications satellite was stationed initially over the Indian Ocean, providing coverage to Europe, Africa, Asia and Australasia through its 44 C- and 12 Ku-band transponders. The Loral FS-1300 satellite had a dry mass of 1978 kg and carried a further 2745 kg of propellant at launch. As of 4 September 2001 located at 56.46 deg E drifting at 0.118 deg E per day. As of 2007 Mar 9 located at 61.96E drifting at 0.002E degrees per day.

2002 February 23 - . 06:59 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L-3 V148.
  • Intelsat 904 - . Mass: 4,680 kg (10,310 lb). Nation: International. Agency: Intelsat. Manufacturer: Palo Alto. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 27380 . COSPAR: 2002-007A. Apogee: 35,800 km (22,200 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Communications satellite. Launch delayed from February 14 and 20. The Ariane 44L placed the Loral FS-1300HL-class Intelsat 904 satellite in a 176 x 35812 km x 7.0 deg geostationary transfer orbit. The spacecraft was to be used for Indian Ocean region communications. Intelsat 904 had a dry mass of 2350 kg and carried 2330 kg of fuel. As of 2007 Mar 9 located at 59.96E drifting at 0.000E degrees per day.

2002 March 30 - . 17:25 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 406-01.
  • Intelsat 903 - . Mass: 4,726 kg (10,419 lb). Nation: International. Agency: Intelsat. Manufacturer: Palo Alto. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 27403 . COSPAR: 2002-016A. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Communications satellite. Moved from Proton M to Proton K booster. Launch delayed from November 26, 2001, and March 4, 2002. The three stage Proton booster put the DM3 upper stage and payload on a suborbital trajectory. The first DM3 burn reached a circular 160 km orbit at 1742 UTC. The second burn at 1838 UTC raised apogee to about 35800 km, and a third burn near apogee at 2339 UTC raised perigee to about 3500 km and lowered inclination to 25 deg. Blok DM3 separated from the Intelsat 903 payload at 0008 UTC on March 31. By April 5, Intelsat 903 was in a 31653 x 35817 km x 0.7 deg near-synchronous orbit. Intelsat 903 had a launch mass of 4726 kg and a dry mass around 2350 kg, and carried C and Ku band antennas. It was built by SS/Loral using a derivative of the FS-1300 platform. As of 2007 Mar 5 located at 34.50W drifting at 0.011W degrees per day.

2002 May 7 - . 17:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 404-02.
  • DirecTV-5 - . Payload: Tempo 1. Mass: 3,640 kg (8,020 lb). Nation: USA. Agency: DirecTV. Manufacturer: Palo Alto. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 27426 . COSPAR: 2002-023A. Apogee: 35,799 km (22,244 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Direct Broadcasting satellite. Launch delayed from October 2000, February, May 21 and October19, 2001, as the user and launch provider moved the payload from Proton to Atlas 2AS and then back again to Proton. The DM3 upper stage made two burns to put the DirecTV satellite in a 6568 x 35809 km x 17.7 deg transfer orbit. The Loral FS-1300 class satellite used its R-4D apogee engine to reach geostationary orbit at 129 W by May 19. The DirecTV satellite broadcasting company was a subsidiary of GM/Hughes. As of 2007 Mar 11 located at 110.11W drifting at 0.004W degrees per day.

2002 June 5 - . 06:44 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L-3 V152.
  • Intelsat 905 - . Mass: 4,723 kg (10,412 lb). Nation: International. Agency: Intelsat. Manufacturer: Palo Alto. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 27438 . COSPAR: 2002-027A. Apogee: 35,799 km (22,244 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Intelsat 905 was launched into a geostationary transfer orbit. The satellite had a mass of 1984 kg with 2739 kg of propellant and was built by Loral for the privatized Intelsat company. It was to be stationed over the Atlantic. The Intelsat 905 satellite used a new version of the venerable General Dynamics R-4D bipropellant engine, the R-4D-15 HiPAT (High Performance Apogee Thruster) with a thrust of 445N. The first two HiPATs were built by Marquardt/Van Nuys, but new ones were built at GD's Redmond site. By June 15, I-905 was in a 35642 x 35793 km x 0.1 deg geostationary drift orbit at 26 deg W. As of 2007 Mar 8 located at 24.48W drifting at 0.007W degrees per day.

2002 August 22 - . 05:15 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 406-02.
  • Echostar 8 - . Mass: 4,660 kg (10,270 lb). Nation: USA. Agency: PanAmSat. Manufacturer: Palo Alto. Program: Echostar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 27501 . COSPAR: 2002-039A. Apogee: 35,799 km (22,244 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Launch delayed from June 16 and 22, July 18, August 2 and 20 due to payload problems. Echostar 8 was an American geostationary communication spacecraft. The 4.7-ton satellite was to provide digital TV broadcast to North America through its 16 spot beams and 41 transponders in the Ku-band after parking over 110 W longitude. As of 2007 Mar 11 located at 110.01W drifting at 0.003W degrees per day.

2002 September 6 - . 06:44 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L-3 V154.
  • Intelsat 906 - . Mass: 4,723 kg (10,412 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 27513 . COSPAR: 2002-041A. Apogee: 35,808 km (22,250 mi). Perigee: 35,765 km (22,223 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Intelsat 906 was a geostationary communications spacecraft of the international Intelsat consortium (privatised as Intelsat Ltd.). It was to provide Internet, telephony, and television broadcasts to Europe, Asia, and Australia through its 72 C- and 22 Ku-band transponders after being parked over 64 E longitude. It replaced Intelsat 804 which was to then be moved to 176 E to handle the increased cross-Atlantic demand. As of 2007 Mar 10 located at 64.19E drifting at 0.001W degrees per day.

2003 February 15 - . 07:00 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L-3 V159.
  • Intelsat 907 - . Payload: LS-1300HL. Mass: 4,685 kg (10,328 lb). Nation: International. Agency: Intelsat. Manufacturer: Palo Alto. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 27683 . COSPAR: 2003-007A. Apogee: 35,789 km (22,238 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Final Ariane 4 launch. Intelsat 907 was scheduled to be in service March 2003 and provide enhanced C-band coverage for the Americas, Africa and Europe and high-power Ku-band spot beam coverage for Europe and Africa. The satellite replaced Intelsat 605 at 332.5 deg E. With more than twice the Ku-band power, Intelsat 907 would support corporate broadcast distribution and broadband applications including high speed Internet access, multicasting and streaming. Users of the new satellite would require 1.0 m Ku-band antennae to access the satellite. Flexible transponder activation allowed use of Ku-Band for 14 out of 16 channels. With a total of up to 76 C-Band 36 MHz equivalent unit transponders, Intelsat 907 provided 19% more capacity than the satellite it replaced. C-band footprints included full coverage of South and Central America, broad coverage over Europe, Africa and the Middle East, and connectivity to North America. As of 2007 Mar 11 located at 27.53W drifting at 0.006W degrees per day.

2003 June 11 - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5G. LV Configuration: Ariane 5G V161 (515).
  • 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: 0.1000 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.

2003 August 8 - . 03:31 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL 10.
  • Echostar 9 (Telstar 13) - . Mass: 4,737 kg (10,443 lb). Nation: USA. Agency: PanAmSat. Program: Echostar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 27854 . COSPAR: 2003-034A. Apogee: 35,809 km (22,250 mi). Perigee: 35,764 km (22,222 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Originally to have launched December 2002. Echostar 9 carried a Ku and Ka band communications payload for Echostar, and a C-band payload owned by Loral Skynet but about to be sold to Intelsat. Loral called the satellite Telstar 13. As of 2007 Mar 10 located at 121.04W drifting at 0.007W degrees per day.

2004 January 11 - . 04:13 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL 12.
  • Estrela do Sul 1 (Skynet Brazil 1, Telstar 14) - . Mass: 4,694 kg (10,348 lb). Nation: Brazil. Agency: Skynet. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28137 . COSPAR: 2004-001A. Apogee: 35,794 km (22,241 mi). Range: 0 km ( mi). Perigee: 35,779 km (22,231 mi). Period: 1,436.10 min. Initially planned for launch on Delta 4M+ (4,2). Launch delayed from January 10. Placed in geosynchronous orbit but reports indicated there were problems deploying one of the solar panels. As of 2007 Mar 11 located at 63.07W drifting at 0.006W degrees per day.

2004 March 13 - . 05:40 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. Launch Pad: SLC36B. LV Family: Atlas V. Launch Vehicle: Atlas IIIA. LV Configuration: Atlas 3A AC-202.
  • MBSAT - . Mass: 4,143 kg (9,133 lb). Nation: Japan. Agency: MBC. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28184 . COSPAR: 2004-007A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Mobile S-band digital broadcasting services for home and automobile users in Japan. As of 2007 Mar 9 located at 144.03E drifting at 0.009W degrees per day..

2004 May 4 - . 12:42 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL.
  • DirecTV 7S - . Mass: 5,483 kg (12,087 lb). Nation: USA. Agency: DirecTV. Manufacturer: Palo Alto. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28238 . COSPAR: 2004-016A. Apogee: 35,792 km (22,240 mi). Perigee: 35,730 km (22,200 mi). Inclination: 0.0000 deg. Period: 1,434.80 min. Summary: Delayed from February 29, May 2. Transferred from Ariane 5 under launch backup agreement. Record single payload to geosynchronous transfer orbit. As of 2007 Mar 11 located at 119.04W drifting at 0.000E degrees per day..

2004 June 29 - . 03:58 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL 11. FAILURE: Partial failure - upper stage left satellite stranded in useless orbit.. Failed Stage: 3.
  • Apstar 5 - . Payload: Apstar 1R, Telstar 18, LS-1300. Mass: 4,640 kg (10,220 lb). Nation: China. Agency: APT. Manufacturer: Palo Alto. Program: Apstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28364 . COSPAR: 2004-024A. Apogee: 35,799 km (22,244 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Delayed from November 2003, April 28 2004. Partial failure (upper stage). As of 2007 Mar 11 located at 138.01E drifting at 0.009W degrees per day..

2005 February 12 - . 21:03 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V164 (521) City of Bremen.
  • 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: 0.1000 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.

2005 February 26 - . 09:25 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 2022. LV Configuration: H-IIA 2022 H-IIA-7F.
  • Himawari 6 - . Payload: MT-Sat 1R. Mass: 3,300 kg (7,200 lb). Nation: Japan. Agency: MLIT. Manufacturer: Palo Alto. Class: Earth. Type: Weather satellite. Spacecraft: FS-1300. USAF Sat Cat: 28622 . COSPAR: 2005-006A. Apogee: 35,798 km (22,243 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.20 min. Return to flight after earlier failure; first commercial mission for H-2A. Delayed from August 2003, January 2004, and February 24, 2005. The dual-purpose satellite was to provide weather data for the Japanese Meteorological Agency (as with others in the Himawari-GMS series), and air traffic control support (airplane-ATC voice/data links, GPS augmentation and airplane position tracking) for the Japanese Civil Aviation Bureau. As of 2007 Mar 11 located at 140.26E drifting at 0.000E degrees per day.

2005 May 22 - . 17:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton M s/n 53510 / Breeze M s/n 88512.
  • DirecTV-8 - . Mass: 3,711 kg (8,181 lb). Nation: USA. Agency: DirecTV. Manufacturer: Palo Alto. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28659 . COSPAR: 2005-019A. Apogee: 35,842 km (22,271 mi). Perigee: 35,711 km (22,189 mi). Inclination: 0.1000 deg. Period: 1,435.60 min. Provided United States direct-television broadcast coverage from the 101 degrees West longitude orbital slot. The satellite carried 16 high-power transponders for high-quality national digital video services. Purchased in October 2003 together with DirecTV-9S for a total price of $220 million for both. As of 2007 Mar 11 located at 100.77W drifting at 0.002W degrees per day.

2005 June 23 - . 14:03 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL 14 (04L?).
  • Intelsat Americas 8 - . Payload: Telstar 8. Mass: 5,500 kg (12,100 lb). Nation: USA. Agency: Intelsat. Manufacturer: Palo Alto. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28702 . COSPAR: 2005-022A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Delayed since 2002; most recently delayed from December 4 and 17, 2004. Communications satellite with Ku-, C- and Ka-band transponders, owned by Intelsat, which had been privatized. As of 2007 Mar 11 located at 89.01W drifting at 0.007W degrees per day..

2005 August 11 - . 08:20 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5GS. LV Configuration: Ariane 5GS V166 (523).
  • 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: 0.0000 deg. Period: 1,436.10 min. Summary: 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..

2006 March 11 - . 22:33 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V170 (527).
  • 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: 0.0000 deg. Period: 1,436.10 min. Summary: 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..

2006 May 27 - . 21:09 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V171 (529).
  • 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: 0.0000 deg. Period: 1,436.10 min. Summary: 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..

2006 June 18 - . 07:50 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL 29.
  • Galaxy 16 - . Payload: LS-1300X. Mass: 4,640 kg (10,220 lb). Nation: USA. Agency: PanAmSat. Manufacturer: Palo Alto. Program: Galaxy. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 29236 . COSPAR: 2006-023A. Apogee: 35,799 km (22,244 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0200 deg. Period: 1,436.11 min. Summary: As of 2007 Mar 11 located at 98.98W drifting at 0.005W degrees per day..

2006 October 13 - . 20:56 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V173 (533).
  • 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: 0.0000 deg. Period: 1,436.10 min. Summary: 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..

2006 December 8 - . 22:08 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V174 (534).
  • 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.

2008 April 14 - . 20:12 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 421. LV Configuration: Atlas V 421 AV-014.
  • ICO G1 - . Mass: 6,600 kg (14,500 lb). Nation: USA. Agency: Martin. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 32763 . COSPAR: 2008-016A. Apogee: 35,800 km (22,200 mi). Perigee: 35,774 km (22,228 mi). Inclination: 6.0000 deg. Period: 1,436.10 min. Summary: The satellite was to provide mobile communications services for ICO Global Communications, a successor company to Teledesic..

2008 May 21 - . 09:43 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL s/n SL30.
  • Galaxy 18 - . Mass: 4,642 kg (10,233 lb). Nation: USA. Agency: Intelsat. Program: Galaxy. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 32951 . COSPAR: 2008-024A. Apogee: 35,799 km (22,244 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Intelsat communications satellite, located at 123 W as a replacement for Galaxy 10R. 24 C-band, and 24 Ku-band transponders serving North American customers..

2008 July 7 - . 21:47 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Protostar 1 / Intelsat 5 - . Payload: Intelsat 5. Mass: 4,100 kg (9,000 lb). Nation: Bermuda. Agency: Arianespace. Class: Communications. Type: 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: 0.0000 deg. Period: 1,436.10 min. Summary: 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..

2008 July 16 - . 05:20 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL s/n SL34.
  • Echostar 11 - . Mass: 5,511 kg (12,149 lb). Nation: USA. Agency: PanAmSat. Manufacturer: Palo Alto. Program: Echostar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 33207 . COSPAR: 2008-035A. Apogee: 35,799 km (22,244 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Satellite provided direct television broadcasting services for the North American Dish Network..

2008 September 24 - . 19:28 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL s/n SL35.
  • Galaxy 19 - . Mass: 4,690 kg (10,330 lb). Nation: USA. Agency: Intelsat. Program: Galaxy. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 33376 . COSPAR: 2008-045A. Apogee: 35,812 km (22,252 mi). Perigee: 35,643 km (22,147 mi). Inclination: 0.1000 deg. Period: 1,433.10 min.

2009 February 26 - . 18:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-3SLB. LV Configuration: Zenit-3SLB s/n LL2.
  • Telstar 11N - . Mass: 4,012 kg (8,844 lb). Nation: Canada. Agency: SIS. Program: Telstar. Spacecraft: FS-1300. USAF Sat Cat: 34111 . COSPAR: 2009-009A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Ku-band direct-broadcast satellite with 39 high-power transponders covering North and Central America, Europe, Africa and the Atlantic Ocean Region, stationed at 37.5 degrees..

2009 June 30 - . 19:10 GMT - . Launch Site: Baikonur. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton/Briz M s/n P346.
  • Sirius FM-5 - . Mass: 5,976 kg (13,174 lb). Nation: USA. Agency: ILS. Program: Sirius. Spacecraft: FS-1300. USAF Sat Cat: 35493 . COSPAR: 2009-034A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Direct radio broadcast satellite for North America. 2900 kg dry mass..

2009 July 1 - . 17:52 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Terrestar-1 - . Mass: 6,910 kg (15,230 lb). Nation: USA. Agency: Arianespace. 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: 5.9000 deg. Period: 1,436.10 min. Summary: Heaviest communications satellite to date; equipped with an 18-meter deployable antenna for S-band mobile communications..

2009 August 11 - . 19:47 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton/Briz M s/n P347.
  • Asiasat 5 - . Mass: 3,760 kg (8,280 lb). Nation: Russia. Agency: ILS. Program: Asiasat. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 35696 . COSPAR: 2009-042A. Apogee: 35,791 km (22,239 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Provided C-band and Ku-band communications services..

2009 September 17 - . 19:19 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton/Briz M s/n P348.
  • Nimiq-5 - . Mass: 4,745 kg (10,460 lb). Nation: Russia. Agency: ILS. Program: Anik. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 35873 . COSPAR: 2009-050A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min.

2009 October 29 - . 20:00 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • NSS 12 - . Mass: 5,620 kg (12,380 lb). Nation: France. Agency: Arianespace. Program: Intelsat. Class: Communications. Type: 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: 0.0000 deg. Period: 1,436.10 min. Summary: C- and Ku-band communications satellite stationed at 57 deg E..

2009 November 23 - . 06:55 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 431. LV Configuration: Atlas V 431 s/n AV024.
  • Intelsat IS-14 - . Mass: 5,663 kg (12,484 lb). Nation: USA. Agency: Martin. Program: Intelsat. Spacecraft: FS-1300. USAF Sat Cat: 36097 . COSPAR: 2009-064A. Apogee: 35,800 km (22,200 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Communications satellite to replace IS-1R at 24 deg W over the Atlantic. The Centaur AV-024 upper stage maneuvered and then released the satellite into a 6157 km x 39094 km x 22.5 deg geosynchronous transfer orbit at 08:53 GMT. IS-14 then used its own propulsion to reach its operational orbit. Mass 2517 kg unfuelled.

2010 March 20 - . 18:26 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton/Briz M s/n P355.
  • Echostar 14 - . Mass: 6,380 kg (14,060 lb). Nation: USA. Agency: ILS. Program: Echostar. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 36499 . COSPAR: 2010-010A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min.

2010 July 10 - . 18:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton/Briz M s/n P358.
  • Echostar 15 - . Mass: 5,520 kg (12,160 lb). Nation: USA. Agency: ILS. Program: Echostar. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 36792 . COSPAR: 2010-034A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.1000 deg. Period: 1,436.00 min. Summary: Supported Dish direct-to-home broadcast network to North America..

2010 October 14 - . 18:53 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton/Briz M.
  • XM-5 - . Payload: Sirius XM-5. Nation: USA. Agency: Sirius. Program: XM. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 37185 . COSPAR: 2010-053A. Apogee: 35,790 km (22,230 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Fifth direct-broadcast digital radio satellite in the Sirius constellation..

2010 November 26 - . 18:39 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Intelsat 17 - . Payload: Intelsat IS-17. Mass: 5,393 kg (11,889 lb). Nation: USA. Program: Intelsat. Class: Communications. Type: 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: 0.0000 deg. Period: 1,436.10 min. Summary: Communications satellite to be stationed at 66 deg E over the Indian Ocean; 5540 kg loaded / 2393 kg unfuelled..

2010 December 29 - . 21:27 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA s/n V199.
  • Hispasat 1E - . Mass: 5,320 kg (11,720 lb). Nation: Spain. Agency: Hispasat. Program: Hispasat. Class: Communications. Type: 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: 0.0000 deg. Period: 1,436.10 min. Summary: Ku band communications; 5320 kg loaded / 2175 kg unfuelled..

2011 May 20 - . 19:15 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton-M/Briz-M.
  • Telstar 14R - . Mass: 4,970 kg (10,950 lb). Nation: USA. Program: Telstar. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. COSPAR: 2011-021A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Ku-band direct-broadcast satellite providing satellite television to Brazil. Failed to fully deploy one of its solar arrays..

2011 September 29 - . 18:32 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton-M/Briz-M.
  • Quetzsat 1 - . Mass: 5,514 kg (12,156 lb). Nation: Mexico. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 37826 . COSPAR: 2011-054A. Apogee: 35,800 km (22,200 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Ku-band communications satellite to be leased to Echostar..

2011 October 19 - . 18:48 GMT - . Launch Site: Baikonur. LV Family: Proton.
  • Viasat 1 - . Mass: 6,740 kg (14,850 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 37843 . COSPAR: 2011-059A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Ka-band broadband data satellite for North American service. Coverage included 9 Canadian spot beams owned by Telesat and 63 US beams owned by ViaSat..

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