Encyclopedia Astronautica
Eurostar 3000


French communications satellite bus. Operational, first launch 2005.03.11 (Inmarsat 4-F1). Third generation of Matra Marconi Space GEO satellite platforms serving mainly commercial telecommunications applications.

First Launch: 2005.03.11.
Last Launch: 2011.09.24.
Number: 23 .

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...
  • 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...
  • 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
  • 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...
  • 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 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...
  • 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 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...

Associated Manufacturers and Agencies
Associated Programs
  • Eutelsat EUTELSAT regional geostationary telecommunication satellite for European countries. Operated by the EUTELSAT organization. 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.
  • JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. 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...
  • 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...
  • 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 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...

Eurostar 3000 Chronology


2005 March 11 - . 21:42 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 AV-004.
  • Inmarsat 4-F1 - . Payload: Inmarsat 4A / Eurostar 3000GM. Mass: 5,959 kg (13,137 lb). Nation: International. Agency: Inmarsat. Manufacturer: EADS Astrium. Program: Inmarsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 28628 . COSPAR: 2005-009A. Apogee: 36,011 km (22,376 mi). Perigee: 35,562 km (22,097 mi). Inclination: 3.0000 deg. Period: 1,436.10 min. Heaviest single payload to geosynchronous transfer orbit to that date. Delayed from October 2004, February 27, March 10, 2005. The satellite was to provide L-band mobile communications and wideband data transmission for Inmarsat's global network. As of 2007 Mar 11 located at 63.82E drifting at 0.000E degrees per day.

2005 September 8 - . 19:53 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton-M/Briz-M 535-12.
  • Anik F1-R - . Payload: Eurostar 3000S. Mass: 4,500 kg (9,900 lb). Nation: Canada. Agency: Telesat. Manufacturer: EADS Astrium. Program: Anik. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 28868 . COSPAR: 2005-036A. Apogee: 35,794 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Moved up from October, delayed from August 9, moved up from September 15 . Telesat Canada communications satellite operating in C- and Ku-band. As of 2007 Mar 10 located at 107.32W drifting at 0.005W degrees per day..

2005 November 8 - . 14:07 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 23.
  • Inmarsat 4F-2 - . Payload: Inmarsat 4B; Eurostar 3000GM. Mass: 5,958 kg (13,135 lb). Nation: USA. Agency: Inmarsat. Program: Inmarsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 28899 . COSPAR: 2005-044A. Apogee: 35,965 km (22,347 mi). Perigee: 35,902 km (22,308 mi). Inclination: 2.9000 deg. Period: 1,443.60 min. Summary: The satellite was fitted with a 10 meter diameter antenna for mobile communications. Payload moved from Ariane 5 EC-A. Launch delayed from September, November 4 and 5, 2005. As of 2007 Mar 11 located at 52.87W drifting at 0.010W degrees per day..

2006 August 4 - . 21:48 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton-M/Briz-M 535-14.
  • Hot Bird 8 - . Mass: 4,875 kg (10,747 lb). Nation: Europe. Agency: Eutelsat. Manufacturer: EADS Astrium. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 29270 . COSPAR: 2006-032A. Apogee: 35,817 km (22,255 mi). Perigee: 35,755 km (22,217 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Ku-band communications direct broadcast satellite to supplement Eutelsat constellation of Hot Birds. As of 2007 Mar 4 located at 13.03E drifting at 0.010E degrees per day..

2007 March 11 - . 22:03 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V175 (535).
  • Skynet 5A - . 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: 0.1000 deg. Period: 1,436.10 min. Summary: 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..

2007 April 9 - . 22:54 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton-M/Briz-M 535-16.
  • Anik F3 - . Payload: Eurostar 3000S. Mass: 4,634 kg (10,216 lb). Nation: Canada. Agency: Telesat. Manufacturer: Friedrichshafen. Program: Anik. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 31102 . COSPAR: 2007-009A. Apogee: 35,795 km (22,241 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.20 min. Summary: Communications satellite with C, Ku and Ka band transponders..

2007 November 14 - . 22:06 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V179 (538).
  • Skynet 5B - . 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: 0.1000 deg. Period: 1,436.10 min. Summary: Skynet 5B was designed to provide communications services in the SHF and UHF bands to the UK Ministry of Defence..

2008 June 12 - . 22:05 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Skynet 5C - . Payload: Eurostr 3000S. 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: 0.6000 deg. Period: 1,436.10 min.

2008 August 18 - . 22:43 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M.
  • Inmarsat 4 F3 - . Mass: 4,960 kg (10,930 lb). Nation: USA. Agency: Inmarsat. Program: Inmarsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 33278 . COSPAR: 2008-039A. Apogee: 36,027 km (22,386 mi). Perigee: 36,009 km (22,374 mi). Inclination: 3.1000 deg. Period: 1,447.90 min. Summary: Maritime communications satellite with a solar panel span of 45 m, and a 10-m diameter L-band mobile communications antenna..

2008 September 19 - . 21:48 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M.
  • Nimiq 4 - . Mass: 4,800 kg (10,500 lb). Nation: Canada. Agency: ILS. Program: Anik. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 33373 . COSPAR: 2008-044A. Apogee: 35,749 km (22,213 mi). Perigee: 35,653 km (22,153 mi). Inclination: 0.1000 deg. Period: 1,431.70 min. Summary: Geostationary television broadcasting satellite launched for Telesat..

2008 November 5 - . 20:44 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M.
  • Astra 1M - . Mass: 5,344 kg (11,781 lb). Nation: Luxembourg. Agency: ILS. Program: Astra. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 33436 . COSPAR: 2008-057A. Apogee: 35,795 km (22,241 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.1000 deg. Period: 1,435.90 min. ASTRA 1M was positioned at Astra's prime 19.2 deg E position, providing pan-European coverage for Direct-to-Home services. Its entry into service would have allowed Astra to redeploy other satellites to its orbital position of 23.5 east. Total power consumption: 9.3 kW BOL, 8.3 kW EOL; Transponder capacity: 36/32 at 26 and 33 MHz; TWTA output power: 150 W; Channel capacity in10.7 - 12.75 GHz: 72 channels (bands D, B, E and F) .

2008 December 20 - . 22:35 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • 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: 0.0000 deg. Period: 1,436.10 min. Summary: Ku-band satellite slated to replace Hot Bird 3 at 13 deg E..

2009 February 11 - . 22:09 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Hot Bird 10 - . Mass: 4,875 kg (10,747 lb). Nation: Europe. Agency: Arianespace. Program: Eutelsat. 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: 0.1000 deg. Period: 1,436.10 min.

2009 October 1 - . 21:59 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Amazonas 2 - . Mass: 5,465 kg (12,048 lb). Nation: France. Agency: Arianespace. Program: Hispasat. Class: Communications. Type: 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: 0.1000 deg. Period: 1,436.10 min. Summary: Commercial broadcast satellite for North and South America..

2010 May 21 - . 22:01 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Astra 3B - . Mass: 5,471 kg (12,061 lb). Nation: Luxembourg. Agency: Arianespace. Program: Astra. Class: Communications. Type: 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: 0.1000 deg. Period: 1,436.10 min. Summary: Communications satellite with 52 Ku-band transponders; stationed at 23.5 deg E..

2010 June 3 - . 22:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M.
  • Arabsat 5B - . Mass: 5,420 kg (11,940 lb). Nation: Russia. Agency: ILS. Program: Arabsat. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 36592 . COSPAR: 2010-025A. Apogee: 35,804 km (22,247 mi). Perigee: 35,767 km (22,224 mi). Inclination: 0.0000 deg. Period: 1,436.00 min. Summary: Direct-to-home broadcast satellite, stationed at 26 deg E..

2010 June 26 - . 21:41 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Coms 1 - . Mass: 2,400 kg (5,200 lb). Nation: Korea South. Agency: Arianespace. Class: Communications. Type: 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: 0.0000 deg. Period: 1,436.10 min. Summary: 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: 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: 0.0000 deg. Period: 1,436.10 min. Summary: Communications satellite with 16 C-band and 24 Ku-band transponders, stationed at 30.5 deg E..

2010 December 26 - . 21:51 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M.
  • Ka Sat - . Payload: KA-SAT . Mass: 6,150 kg (13,550 lb). Nation: Europe. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 37258 . COSPAR: 2010-069A. Apogee: 35,788 km (22,237 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Ka band communications with 80 spot beams; 6150 kg loaded / 3200 kg unfuelled..

2011 April 22 - . 21:37 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Yahsat 1A - . Nation: UAE. Class: Communications. Type: 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: 0.0000 deg. Period: 1,436.10 min. Summary: 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..

2011 August 6 - . 22:52 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Astra 1N - . Nation: Luxembourg. Program: Astra. Class: Communications. Type: 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: 0.0000 deg. Period: 1,436.00 min. Summary: Geosynchronous communications satellite to be stationed at 19.2 deg E for direct television broadcasting to Europe..

2011 September 21 - . 21:38 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Arabsat 5C - . Nation: Arab States. Program: Arabsat. Class: Communications. Type: 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: 0.1000 deg. Period: 1,436.10 min. Summary: C-band/Ka-band communications satellite for television broadcast to Arab countries..

2011 September 24 - . 20:18 GMT - . Launch Site: Kiritimati. Launch Platform: Odyssey. LV Family: Zenit. Launch Vehicle: Zenit-3SL.
  • Atlantic Bird 7 - . Nation: Europe. Program: Eutelsat. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 37816 . COSPAR: 2011-051A. Apogee: 35,804 km (22,247 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Eutelsat's communications satellite. First mission by Sea Launch from the Odyssey floating launch platform after emerging from bankruptcy..

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