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Arianespace

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AKA: AE.

• Spacenet F3 - . Mass: 600 kg (1,320 lb). Nation: USA. Agency: Arianespace. Manufacturer: Lockheed. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000.

• Oscar 19 - . Payload: LuSat. Mass: 12 kg (26 lb). Nation: Argentina. Agency: Arianespace. Program: Oscar. Class: Communications. Type: Amateur radio communications satellite. Spacecraft: Oscar. USAF Sat Cat: 20442 . COSPAR: 1990-005G. Apogee: 797 km (495 mi). Perigee: 779 km (484 mi). Inclination: 98.6000 deg. Period: 100.60 min. Carried CCD camera..

• Oscar 16 - . Payload: PACSAT. Mass: 12 kg (26 lb). Nation: USA. Agency: Arianespace. Program: Oscar. Class: Communications. Type: Amateur radio communications satellite. Spacecraft: Oscar. USAF Sat Cat: 20439 . COSPAR: 1990-005D. Apogee: 797 km (495 mi). Perigee: 781 km (485 mi). Inclination: 98.6000 deg. Period: 100.60 min. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

• Oscar 17 - . Payload: Microsat 2. Mass: 12 kg (26 lb). Nation: Brazil. Agency: Arianespace. Program: Oscar. Class: Communications. Type: Amateur radio communications satellite. Spacecraft: Oscar. USAF Sat Cat: 20440 . COSPAR: 1990-005E. Apogee: 796 km (494 mi). Perigee: 780 km (480 mi). Inclination: 98.6000 deg. Period: 100.60 min.

• BS 2X - . Payload: BS 2X. Mass: 2,800 kg (6,100 lb). Nation: USA. Agency: Arianespace. Program: BS. Spacecraft: HS 376. Apogee: 9.00 km (5.50 mi).

• Turksat 1A - . Payload: Turksat 1A. Mass: 1,890 kg (4,160 lb). Nation: Turkey. Agency: Arianespace. Program: Turksat. Spacecraft: Spacebus 2000.

• Telstar 402 - . Mass: 3,415 kg (7,528 lb). Nation: USA. Agency: Arianespace. Manufacturer: Lockheed. Program: Telstar series. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 7000. Decay Date: 2004-11-14 . USAF Sat Cat: 23249 . COSPAR: 1994-058A. Apogee: 19,340 km (12,010 mi). Perigee: 292 km (181 mi). Inclination: 7.1000 deg. Period: 341.80 min.

• Equator-S - . Nation: Germany. Agency: Arianespace. Manufacturer: Max-Planck-Institut. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Equator-S. USAF Sat Cat: 25068 . COSPAR: 1997-075B. Apogee: 67,065 km (41,672 mi). Perigee: 591 km (367 mi). Inclination: 6.2000 deg. Period: 1,337.20 min.

• ST-1 - . Payload: Eurostar 2000+. Mass: 3,200 kg (7,000 lb). Nation: Singapore. Agency: Arianespace. Manufacturer: Toulouse. Program: Singapore, Taiwan. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 2000 . USAF Sat Cat: 25460 . COSPAR: 1998-049A. Apogee: 35,804 km (22,247 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.1000 deg. Period: 1,436.10 min.

  Singapore-Taiwan-1 Matra Marconi Space Eurostar 2000 class satellite to provide communications for Singapore Telecom and Chunghwa Telecom of Taiwan. Geostationary at 88.0 degrees E. Positioned in geosynchronous orbit at 88 deg E in 1998-1999 As of 5 September 2001 located at 88.04 deg E drifting at 0.009 deg W per day. As of 2007 Mar 10 located at 88.05E drifting at 0.007W degrees per day.

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

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

• Orion 2 - . Mass: 3,814 kg (8,408 lb). 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.

• STRV-1d - . Mass: 4,758 kg (10,489 lb). Nation: UK. Agency: Arianespace. Manufacturer: Farnborough. Class: Technology. Type: Navigation technology satellite. Spacecraft: STRV. USAF Sat Cat: 26611 . COSPAR: 2000-072D. Apogee: 39,282 km (24,408 mi). Perigee: 605 km (375 mi). Inclination: 7.1000 deg. Period: 708.30 min.

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

• STRV-1c - . Mass: 4,758 kg (10,489 lb). Nation: UK. Agency: Arianespace. Manufacturer: Farnborough. Class: Technology. Type: Navigation technology satellite. Spacecraft: STRV. USAF Sat Cat: 26610 . COSPAR: 2000-072C. Apogee: 39,218 km (24,368 mi). Perigee: 636 km (395 mi). Inclination: 6.3400 deg. Period: 707.65 min.

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

• Envisat - . Mass: 7,991 kg (17,617 lb). Nation: Europe. Agency: Arianespace. Class: Earth. Type: Earth resources radar satellite. Spacecraft Bus: SPOT-4. Spacecraft: Envisat. USAF Sat Cat: 27386 . COSPAR: 2002-009A. Apogee: 785 km (487 mi). Perigee: 783 km (486 mi). Inclination: 98.6000 deg. Period: 100.50 min.

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

• 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.

• Nanosat 01 - . Mass: 20 kg (44 lb). Nation: Spain. Agency: Arianespace. Manufacturer: INTA. Class: Technology. Type: Navigation technology satellite. Spacecraft: Nanosat 01. USAF Sat Cat: 28493 . COSPAR: 2004-049B. Apogee: 666 km (413 mi). Perigee: 658 km (408 mi). Inclination: 98.1000 deg. Period: 98.00 min. Experimental nanosat built by the Spanish space agency (INTA)..

• 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.

• ATV-1 Jules Verne - . Mass: 19,012 kg (41,914 lb). Nation: France. Agency: Arianespace. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: ATV. Duration: 204.39 days. Decay Date: 2008-09-29 . USAF Sat Cat: 32686 . COSPAR: 2008-008A. Apogee: 343 km (213 mi). Perigee: 336 km (208 mi). Inclination: 51.6000 deg. Period: 91.30 min.

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

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

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

• Vinasat 1 - . Payload: A2100A. Mass: 6,740 kg (14,850 lb). Nation: Vietnam. Agency: Arianespace. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 32767 . COSPAR: 2008-018A. Apogee: 35,789 km (22,238 mi). Perigee: 35,787 km (22,236 mi). Inclination: 0.0000 deg. Period: 1,436.20 min. First satellite launched by Vietnam. The Vietnam Post and Telecom Corporation communications satellite was equipped with C and Ku band payloads..

• Star One C2 - . Payload: Spacebus 3000B3. Mass: 4,100 kg (9,000 lb). Nation: Brazil. Agency: Arianespace. Program: Brasilsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 32768 . COSPAR: 2008-018B. Apogee: 35,790 km (22,230 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Communications satellite owned by Brazilian operator Star One with C, Ku and X-band transponders.

• Skynet 5C - . Payload: Eurostar 3000S. Mass: 4,638 kg (10,225 lb). Nation: UK. Agency: Arianespace. Program: Skynet. Class: Communications. Type: Military communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 33055 . COSPAR: 2008-030A. Apogee: 35,801 km (22,245 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.6000 deg. Period: 1,436.10 min.

• Turksat 3A - . Payload: Spacebus 4000B2. Mass: 3,110 kg (6,850 lb). Nation: Turkey. Agency: Arianespace. Program: Turksat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 33056 . COSPAR: 2008-030B. Apogee: 35,811 km (22,251 mi). Perigee: 35,761 km (22,220 mi). Inclination: 0.0000 deg. Period: 1,436.00 min. Replacement for Turksat-1C, positioned at 42 deg E; 24 Ku-band transponders..

• Protostar 1 / Intelsat 5 - . Payload: Intelsat 5. Mass: 4,100 kg (9,000 lb). Nation: Bermuda. Agency: Arianespace. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 33153 . COSPAR: 2008-034A. Apogee: 35,793 km (22,240 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Originally Chinasat 8; sale cancelled due to new US export regulations. Sold to Protostar in 2006, still to serve Chinese market. After launch when Protostar closed down sold to Intelsat and entered service as Intelsat 5..

• Badr 6 - . Mass: 52 kg (114 lb). Nation: Pakistan. Agency: Arianespace. Class: Communications. Type: Military communications satellite. Spacecraft: Badr. USAF Sat Cat: 33154 . COSPAR: 2008-034B. Apogee: 35,801 km (22,245 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.1000 deg. Period: 1,436.10 min.

• Superbird 7 - . Mass: 4,820 kg (10,620 lb). Nation: Japan. Agency: Arianespace. Program: Superbird. Class: Communications. Type: Civilian communications satellite. Spacecraft: DS2000. USAF Sat Cat: 33274 . COSPAR: 2008-038A. Apogee: 35,804 km (22,247 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Ku-band Mitsubishi Electric DS2000 class satellite for Japanese television broadcasting..

• AMC 21 - . Mass: 2,500 kg (5,500 lb). Nation: France. Agency: Arianespace. Program: Americom. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 33277 . COSPAR: 2008-038D. Apogee: 35,677 km (22,168 mi). Perigee: 276 km (171 mi). Inclination: 2.1000 deg. Period: 630.40 min. Ku-band satellite for SES Americom's North American services, using an Orbital Star 2 bus and a Thales Alenia communications payload..

• Hot Bird 9 - . Mass: 4,880 kg (10,750 lb). Nation: France. Agency: Arianespace. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 33459 . COSPAR: 2008-065A. Apogee: 35,792 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Ku-band satellite slated to replace Hot Bird 3 at 13 deg E..

• Eutelsat W2M - . Mass: 3,460 kg (7,620 lb). Nation: France. Agency: Arianespace. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-3K. USAF Sat Cat: 33460 . COSPAR: 2008-065B. Apogee: 35,843 km (22,271 mi). Perigee: 35,735 km (22,204 mi). Inclination: 0.1000 deg. Period: 1,436.20 min. Ku-band satellite designed to operate at 10 deg E. It used the Indian Insat I3K bus and was the first foreign sale of an Indian-built satellite. It made it to geosynchronous orbit but suffered a power system and was written off eight days after launch..

• NSS 9 - . Mass: 2,400 kg (5,200 lb). Nation: Netherlands. Agency: Arianespace. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 33749 . COSPAR: 2009-008A. Apogee: 35,793 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min.

• Hot Bird 10 - . Mass: 4,875 kg (10,747 lb). Nation: Europe. Agency: Arianespace. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 33750 . COSPAR: 2009-008B. Apogee: 35,804 km (22,247 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.1000 deg. Period: 1,436.10 min.

• Spirale A - . Mass: 117 kg (257 lb). Nation: France. Agency: Arianespace. Class: Surveillance. Type: Early warning satellite. Spacecraft: Myriade. USAF Sat Cat: 33751 . COSPAR: 2009-008C. Apogee: 35,693 km (22,178 mi). Perigee: 631 km (392 mi). Inclination: 1.8000 deg. Period: 637.60 min. Demonstrator to prove infrared sensors designed to detect ballistic missile launches and other military targets..

• Spirale B - . Mass: 117 kg (257 lb). Nation: France. Agency: Arianespace. Class: Surveillance. Type: Early warning satellite. Spacecraft: Myriade. USAF Sat Cat: 33752 . COSPAR: 2009-008D. Apogee: 35,681 km (22,171 mi). Perigee: 641 km (398 mi). Inclination: 1.8000 deg. Period: 637.60 min.

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

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

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

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

• Terrestar-1 - . Mass: 6,910 kg (15,230 lb). Nation: USA. Agency: Arianespace. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 35496 . COSPAR: 2009-035A. Apogee: 35,790 km (22,230 mi). Perigee: 35,783 km (22,234 mi). Inclination: 5.9000 deg. Period: 1,436.10 min. Heaviest communications satellite to date; equipped with an 18-meter deployable antenna for S-band mobile communications..

• JCSAT 12 - . Payload: A2100AXS. Mass: 4,000 kg (8,800 lb). Nation: France. Agency: Arianespace. Program: JCSAT. Class: Communications. Type: Communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 35755 . COSPAR: 2009-044A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min.

• Optus D3 - . Payload: Star-2.4. Nation: France. Agency: Arianespace. Program: Aussat. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 35756 . COSPAR: 2009-044B. Apogee: 35,800 km (22,200 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min.

• COMSATBw-1 - . Payload: Spacebus 3000B2. Mass: 2,440 kg (5,370 lb). Nation: France. Agency: Arianespace. Program: COMSATBw. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 35942 . COSPAR: 2009-054A. Apogee: 35,807 km (22,249 mi). Perigee: 35,765 km (22,223 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. German military communications satellite. Dry mass 1040 kg..

• Amazonas 2 - . Mass: 5,465 kg (12,048 lb). Nation: France. Agency: Arianespace. Program: Hispasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 35943 . COSPAR: 2009-054B. Apogee: 35,794 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Commercial broadcast satellite for North and South America..

• NSS 12 - . Mass: 5,620 kg (12,380 lb). Nation: France. Agency: Arianespace. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 36032 . COSPAR: 2009-058A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. C- and Ku-band communications satellite stationed at 57 deg E..

• Thor 6 - . Payload: Spacebus 4000B2. Mass: 3,050 kg (6,720 lb). Nation: France. Agency: Arianespace. Program: Thor Comsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 36033 . COSPAR: 2009-058B. Apogee: 35,793 km (22,240 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Direct broadcast satellite stationed at 1 deg W..

• Helios 2B - . Mass: 4,200 kg (9,200 lb). Nation: France. Agency: Arianespace. Program: Helios. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: SPOT-5A-5B. USAF Sat Cat: 36124 . COSPAR: 2009-073A. Apogee: 680 km (420 mi). Perigee: 680 km (420 mi). Inclination: 98.0000 deg. French military surveillance satellite..

• Astra 3B - . Mass: 5,471 kg (12,061 lb). Nation: Luxembourg. Agency: Arianespace. Program: Astra. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 36581 . COSPAR: 2010-021A. Apogee: 35,807 km (22,249 mi). Perigee: 35,765 km (22,223 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Communications satellite with 52 Ku-band transponders; stationed at 23.5 deg E..

• ComsatBW-2 - . Payload: Spacebus 3000B2. Mass: 2,440 kg (5,370 lb). Nation: Germany. Agency: Arianespace. Program: COMSATBw. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 36582 . COSPAR: 2010-021B. Apogee: 35,792 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. German military communications satellite..

• Coms 1 - . Mass: 2,400 kg (5,200 lb). Nation: Korea South. Agency: Arianespace. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 36744 . COSPAR: 2010-032A. Apogee: 35,789 km (22,238 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Communication, Ocean and Meteorological Satellite. Weather, oceanography, and communications payloads..

• Arabsat 5A - . Mass: 4,800 kg (10,500 lb). Nation: Arab States. Agency: Arianespace. Program: Arabsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 36745 . COSPAR: 2010-032B. Apogee: 35,789 km (22,238 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Communications satellite with 16 C-band and 24 Ku-band transponders, stationed at 30.5 deg E..

• Nilesat 201 - . Payload: Spacebus 4000B2. Mass: 3,200 kg (7,000 lb). Nation: Egypt. Agency: Arianespace. Program: Nilesat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 36830 . COSPAR: 2010-037A. Apogee: 35,804 km (22,247 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Ku-band/Ka-band direct broadcasting satellite..

• Rascom QAF 1R - . Payload: RascomQAF-1R. Mass: 3,050 kg (6,720 lb). Nation: Nigeria. Agency: Arianespace. Program: Rascom. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 36831 . COSPAR: 2010-037B. Apogee: 35,804 km (22,247 mi). Perigee: 35,769 km (22,225 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Ku and C band transponders to provide telecommunications, broadcasting and internet service to Africa for the Regional African Satellite Communications Organization..