Orion 1 Credit: Manufacturer Image |
AKA: Afristar;Asiastar. Status: Operational 1988. First Launch: 1988-03-11. Last Launch: 2006-11-08. Number: 24 . Gross mass: 3,000 kg (6,600 lb).
The Eurostar 2000 platform was the second generation of Matra Marconi Space GEO satellite platforms serving mainly commercial telecommunications applications. The Eurostar 2000 bus was available in both basic and enhanced (Eurostar 2000+) versions. The platform was designed for high performance, reliability and cost effectiveness.
The main features of Eurostar included high versatility (2 to 6 metric tons launch mass, flexible power range) substantial payload accommodation, stable and accurate pointing and high autonomy. The Eurostar 2000 series were built at Marconi's facility in Toulouse, France. The Eurostar series could meet customer needs for fixed services/broadcast, mobile services, and interactive broadband and military applications.
Specification, Eurostar 2000 basic:. Dry mass 1200-1900 kg; launch mass 1600-2300 kg; payload mass 400 kg; payload available power 2-4 kw; 3 Axis stabilization; chemical bi-propellant propulsion. Mission lifetime 12 years.
Specification, Eurostar 2000 plus:. Dry mass 1750-2850 kg; launch mass 2300-3400 kg; payload mass 550 kg; payload available power 4-7 kw; 3 Axis stabilization; chemical bi-propellant propulsion with plasma, ion capability. Mission lifetime 12 years.
TTlTcom 2A, 2B, 2C, 2D Null |
Hispasat 1A, 1B Communication satellite built by Matra Marconi for Hispasat, Spain. Launched 1992 - 1993. Used the Eurostar-2000 bus. |
Orion 1 / Telstar 11 Null |
Hot Bird 2, 3, 4, 5 / Eurobird 2, 9&rarr Null |
4, 10, 16 / Atlantic Bird 4 Null |
Nilesat 101, 102 Communication satellite built by Astrium for Nilesat, Egypt. Launched 1998 - 2000. Used the Eurostar-2000 bus. |
ST 1 Communication satellite built by Astrium for Singapore Telecom (SingTel), Chunghwa Telecom, Singapore. Launched 1998. Used the Eurostar-2000+ bus. |
AfriStar 1, 2, AsiaStar, WorldStar 4 Communication satellite built by Alcatel Space (prime), Astrium (bus) for WorldSpace Corp., USA. Launched 1998 - 2000. Used the Eurostar-2000+ bus. |
Eutelsat W1 / Eurobird 4A / Eutelsat 4A Null |
Astra 2B Communication (Direct Broadcasting) satellite built by Astrium for SES, Luxembourg. Launched 2000. Used the Eurostar-2000+ bus. |
Hot Bird 7 Communication (Direct Broadcasting) satellite built by Astrium for Eutelsat, International. Launched 2002. Used the Eurostar-2000+ bus. |
HellasSat 2 Communication satellite built by Astrium for Hellas Sat, Greece. Launched 2003. Used the Eurostar-2000+ bus. |
Arabsat 4A, 4B, 4AR / Badr 1, 4, 6 Null |
Afristar Credit: Manufacturer Image |
Badr 4 ARABSAT 4B Credit: Manufacturer Image |
Astra 2B Credit: Manufacturer Image |
Eutelsat W1 Credit: Manufacturer Image |
Hellas Sat 2 Credit: Manufacturer Image |
Hispasat 1A Credit: Manufacturer Image |
Hot Bird 2 Credit: Manufacturer Image |
Hot Bird 7 Credit: Manufacturer Image |
Nilesat 1 Credit: Manufacturer Image |
ST-1 Credit: Manufacturer Image |
Telecom 2A Credit: Manufacturer Image |
GE 5 Credit: Manufacturer Image |
French domestic communications; 5 deg E. Communications satellite. Registration France 1984-2.B (Telecom 1A) 1985-2.B (Telecom 1B). 1988-1-C (Telecom 1C). Positioned in geosynchronous orbit at 5 deg W in 1988-1992; 3 deg E in 1992-1996 As of 5 September 2001 located at 109.19 deg W drifting at 8.404 deg W per day. As of 2007 Mar 10 located at 34.65E drifting at 8.341W degrees per day.
French communications; 3 deg E. Positioned in geosynchronous orbit at 3 deg E in 1992; 8 deg W in 1992-1999 As of 5 September 2001 located at 8.05 deg W drifting at 0.004 deg W per day. As of 2007 Mar 11 located at 111.59E drifting at 4.763W degrees per day.
34 Ku-band transponders for TV. Stationed at 37.48 deg W. Launch vehicle put payload into supersynchronous earth orbit with IFR trajectory option. Positioned in geosynchronous orbit at 37 deg W in 1994-1999 As of 5 September 2001 located at 37.54 deg W drifting at 0.010 deg W per day. As of 2007 Mar 11 located at 37.60W drifting at 0.015W degrees per day.
Geostationary at 13.0E. Launch vehicle put payload into supersynchronous earth orbit with IFR/MRS trajectory option. Positioned in geosynchronous orbit at 13 deg E in 1997-1999 As of 3 September 2001 located at 12.95 deg E drifting at 0.024 deg E per day. As of 2007 Mar 4 located at 13.07E drifting at 0.011E degrees per day.
Egypt's first satellite. Geostationary at 7.0 degrees W. Positioned in geosynchronous orbit at 7 deg W in 1998-1999 As of 5 September 2001 located at 6.95 deg W drifting at 0.003 deg W per day. As of 2007 Mar 10 located at 7.00W drifting at 0.007W degrees per day.
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.
Afristar was the first WorldSpace satellite. Afristar was to broadcast digital radio over Africa and the Middle East. Small hand-held radios could pick up the 24 to 96 radio channels available on the three L-band beams. Dry mass of Afristar was 1205 kg; it carried 1534 kg of propellant at launch. Geostationary at 21.0 degrees E. Positioned in geosynchronous orbit at 21 deg E in 1998-1999 As of 3 September 2001 located at 20.98 deg E drifting at 0.004 deg W per day. As of 2007 Mar 10 located at 20.98E drifting at 0.010W degrees per day.
Satellite was originally built as a backup for Argentina's Nahuelsat. This allowed Dornier and Alcatel to deliver the satellite in a record twelve months. Dry mass of GE 5 was 769 kg - it carried 950 kg of propellant at launch. Geostationary at 36.4 degrees W. Positioned in geosynchronous orbit at 79 deg W in 1998-1999 As of 3 September 2001 located at 79.00 deg W drifting at 0.004 deg W per day. As of 2007 Mar 10 located at 78.99W drifting at 0.011W degrees per day.
Direct Radio Broadcasting satelllite. First night launch of Ariane 5. Worldspace's second digital radio satellite. Joined Afristar in orbit with a mission of providing radio broadcasting to the developing world. Stationed at 105 deg E. Positioned in geosynchronous orbit at 105 deg E in 2000. As of 4 September 2001 located at 104.96 deg E drifting at 0.015 deg W per day. As of 2007 Mar 9 located at 104.99E drifting at 0.012W degrees per day.
Geosynchronous communications satellite of the Egyptian company Nilesat SA. The satellite joined Nilesat 101 in providing Ku-band broadcast services. Stationed at 7 deg W. Positioned in geosynchronous orbit at 7 deg W in 2000. As of 2 September 2001 located at 6.98 deg W drifting at 0.002 deg W per day. As of 2007 Mar 9 located at 6.97W drifting at 0.004W degrees per day.
European Telecommunications Satellite Organization's Eutelsat W1 was launched into a geostationary transfer orbit, targetted for a final 10 deg E orbital position. The box-shaped 2.5 x 5.0 m satellite has two rectangular solar panel arrays spanning 31.7m and two dishes, a European beam and a steerable beam. The payload includes 28 Ku-band transponders. Stationed at 10 deg E. Positioned in geosynchronous orbit at 1 deg E in 2000. As of 1 September 2001 located at 9.92 deg E drifting at 0.005 deg E per day. As of 2007 Mar 8 located at 10.05E drifting at 0.006W degrees per day.
Direct Broadcasting satellite. Launch postponed from July 25. Astra 2B was an Astrium/Toulouse Eurostar 2000+ television broadcast satellite owned by the Luxembourg-based Societe Europeene de Satellites. The satellite was to be stationed at 28.2E to replace the German DFS Kopernikus. It carried 28 Ku-band transponders. By September 19 Astra 2B was in a 31,153 x 35,762 km x 0.3 deg orbit, approaching geosynchronous altitude. Stationed at 28 deg E. Positioned in geosynchronous orbit at 28 deg E in 2000. As of 20 August 2001 located at 28.50 deg E drifting at 0.011 deg E per day. As of 2007 Mar 10 located at 28.15E drifting at 0.017W degrees per day.