Eutelsat
Program: Eutelsat. Objective: Communications. Overview: EUTELSAT regional geostationary telecommunication satellite for European countries. Operated by the EUTELSAT organization.
Major Events:

  • 1983 June 16 - Eutelsat 1.  Spacecraft: ECS/OTS. Mass: 1,050 kg (2,310 lb). Launch Site: Kourou. Launch Vehicle: Ariane 1.

    Designator ESA/83/4. Launch time 1159 GMT. Launch agency ESA. Geostationary position 10+/- 0.1 deg E. EUTELSAT 1 is a regional geostationary telecommunication Satellite for European countries. It is operated by the EUTELSAT organization. Frequency plan: 1 36-138 MHz (S-E). 148-149.9 MHz (E-S). 10.7-11.7 GHz (S-E). 14-14.5 GHz (E-S). Positions: Document Positioned in geosynchronous orbit at 10 deg E in 1983; 13 deg E in 1983-1989; 16 deg E in 1989-1991; 25 deg E in 1992-1993; 48E1993-1996; 36 deg E in 1996 As of 31 August 2001 located at 12.27 deg W drifting at 5.043 deg W per day. As of 2007 Mar 9 located at 109.78W drifting at 5.059W degrees per day.

  • 1984 August 4 - Eutelsat 2.  Spacecraft: ECS/OTS. Mass: 700 kg (1,540 lb). Launch Site: Kourou. Launch Vehicle: Ariane 2/3.

    Stationed at 7 deg E. Launch time 1333 UT. Geostationary orbit position 10 +/- 0.1; afterwards 7 +/- 0.1 deg E. EUTELSAT 2 is a regional geostationary satellite for European countries. Positioned in geosynchronous orbit at 10 deg E in 1984; 7 deg E in 1984-1990; 2 deg E in 1991; 1 deg E in 1992-1993 As of 5 September 2001 located at 62.27 deg W drifting at 5.317 deg W per day. As of 2007 Mar 9 located at 57.69E drifting at 5.323W degrees per day.

  • 1985 September 12 - Eutelsat 3.  Spacecraft: ECS/OTS. Launch Site: Kourou. Launch Vehicle: Ariane 2/3.

    Launched with Spacenet F3.

  • 1987 September 16 - Eutelsat I F4.  Spacecraft: ECS/OTS. Mass: 1,175 kg (2,590 lb). Launch Site: Kourou. Launch Vehicle: Ariane 2/3.

    European communications; 10 deg E. Positioned in geosynchronous orbit at 10 deg E in 1987-1988; 13 deg E in 1989-1991; 7 deg E in 1991-1993; 25 deg E in 1993-1999 As of 2 September 2001 located at 33.14 deg E drifting at 0.002 deg E per day. As of 2007 Mar 11 located at 120.92E drifting at 5.702W degrees per day.

  • 1988 July 21 - Eutelsat I F5.  Spacecraft: ECS/OTS. Mass: 1,185 kg (2,612 lb). Launch Site: Kourou. Launch Vehicle: Ariane 2/3.

    European communications; 13 deg E. ECS-5/Eutelsat I F5 is a regional geostationary telecommunications satellite for European countries. It is operated by the EUTELSAT organization. Frequency plan 136-138 MHz (S-E), 148-149.9 MHz (E-S), 10.7-11.7 GHz (S-E), 14.0-14.5 GHz (E-S). Launch time 2334:00 UT. ESA designator ESA/88/03. Positioned in geosynchronous orbit at 10 deg E in 1989-1991; 21 deg E in 1991-1998; 12 deg W in 1998-1999 As of 4 September 2001 located at 48.15 deg E drifting at 7.596 deg W per day. As of 2007 Mar 9 located at 102.26W drifting at 7.597W degrees per day.

  • 1990 August 30 - Eutelsat II F1.  Spacecraft: Spacebus 100. Mass: 1,878 kg (4,140 lb). Launch Site: Kourou. Launch Vehicle: Ariane 44LP.

    Stationed at 13 deg E. Telecommunications satellite. Registered by France in ST/SG/SER.E/234 and 239 until EUTELSAT can register the satellite. EUTELSAT is the European Telecommunications Satellite Organization. Positioned in geosynchronous orbit at 13 deg E in 1990-1998; 48 deg E in 1999. As of 26 August 2001 located at 48.45 deg E drifting at 0.011 deg E per day. As of 2007 Mar 9 located at 6.45E drifting at 3.328W degrees per day.

  • 1991 January 15 - Eutelsat II F2.  Spacecraft: Spacebus 100. Mass: 1,878 kg (4,140 lb). Launch Site: Kourou. Launch Vehicle: Ariane 44L.

    Stationed at 10 deg E. Telecommunications satellite. Registered by France in ST/SG/SER.E/234 and 239 until EUTELSAT can register the satellite. EUTELSAT is the European Telecommunications Satellite Organization. Positioned in geosynchronous orbit at 10 deg E in 1991-1999 12 deg W in 1999-2000 As of 4 September 2001 located at 12.60 deg W drifting at 0.009 deg W per day. As of 2007 Mar 10 located at 28.49E drifting at 4.801W degrees per day.

  • 1991 December 7 - Eutelsat II F3.  Spacecraft: Spacebus 100. Mass: 1,874 kg (4,131 lb). Launch Site: Cape Canaveral. Launch Vehicle: Atlas II.

    Stationed at 16 deg E. Telecommunications satellite. French registration 1991-8. Transfer orbit was 663 min, 200 x 36000 km x 7.0 deg. Registered by France in ST/SG/SER.E/249 until EUTELSAT can register the satellite. EUTELSAT is the European Telecommunications Satellite Organi zation. Launch vehicle put payload into supersynchronous earth orbit with IFR trajectory option. Positioned in geosynchronous orbit at 16 deg E in 1992-1998; 36 deg E in 1999. As of 1 September 2001 located at 21.51 deg E drifting at 0.017 deg E per day. As of 2007 Mar 11 located at 74.40E drifting at 3.531W degrees per day.

  • 1992 July 9 - Eutelsat II F4.  Spacecraft: Spacebus 100. Mass: 1,877 kg (4,138 lb). Launch Site: Kourou. Launch Vehicle: Ariane 44L.

    Stationed at 7 deg E. Positioned in geosynchronous orbit at 7 deg E in 1992-1999; 10 deg E in 1999. As of 3 September 2001 located at 25.62 deg E drifting at 0.019 deg E per day. As of 2007 Mar 10 located at 120.18E drifting at 4.301W degrees per day.

  • 1994 January 24 - Eutelsat II F5.  Spacecraft: Spacebus 100. Mass: 1,880 kg (4,140 lb). Launch Site: Kourou. Launch Vehicle: Ariane 44LP.

    Launched with Turksat 1.

  • 1995 March 28 - Hot Bird 1.  Spacecraft: Spacebus 2000. Mass: 1,800 kg (3,900 lb). Launch Site: Kourou. Launch Vehicle: Ariane 44LP.

    Stationed at 13.0 deg E. Positioned in geosynchronous orbit at 13 deg E in 1995-1999 As of 3 September 2001 located at 12.93 deg E drifting at 0.014 deg E per day. As of 2007 Mar 11 located at 160.81W drifting at 3.441W degrees per day.

  • 1996 November 21 - Hot Bird 2.  Spacecraft: Eurostar 2000. Launch Site: Cape Canaveral. Launch Vehicle: Atlas IIA.

    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.

  • 1997 September 2 - Hot Bird 3.  Spacecraft: Eurostar 2000. Launch Site: Kourou. Launch Vehicle: Ariane 44LP.

    Geosynchronous. Stationed over 13.3E Positioned in geosynchronous orbit at 13 deg E in 1997-1999 As of 3 September 2001 located at 12.96 deg E drifting at 0.012 deg E per day. As of 2007 Mar 11 located at 3.94E drifting at 0.003W degrees per day.

  • 1998 February 27 - Hot Bird 4.  Spacecraft: Eurostar 2000. Launch Site: Kourou. Launch Vehicle: Ariane 42P.

    Geostationary at 13.0 degrees E. Positioned in geosynchronous orbit at 13 deg E in 1998-1999 As of 2 June 2001 located at 14.35 deg E drifting at 0.065 deg E per day. As of 2007 Mar 9 located at 7.18W drifting at 0.004W degrees per day.

  • 1998 October 5 - Eutelsat W2.  Spacecraft: Spacebus 3000. Launch Site: Kourou. Launch Vehicle: Ariane 44L.

    Geostationary at 16.0 degrees E. Positioned in geosynchronous orbit at 16 deg E in 1998-1999 As of 4 September 2001 located at 16.17 deg E drifting at 0.015 deg E per day. As of 2007 Mar 11 located at 16.01E drifting at 0.008W degrees per day.

  • 1998 October 9 - Hot Bird 5.  Spacecraft: Eurostar 2000. Mass: 3,000 kg (6,600 lb). Launch Site: Cape Canaveral. Launch Vehicle: Atlas IIA.

    Geostationary at 10.0 degrees E. Positioned in geosynchronous orbit at 13 deg E in 1998-1999 As of 3 September 2001 located at 12.97 deg E drifting at 0.010 deg E per day. As of 2007 Mar 11 located at 25.56E drifting at 0.014W degrees per day.

  • 1999 April 12 - Eutelsat W3.  Spacecraft: Spacebus 3000. Launch Site: Cape Canaveral. Launch Vehicle: Atlas IIAS.

    Communications satellite is for the European Telecommunications Satellite Organization. The vehicle entered a 153 km x 385 km x 27.4 deg parking orbit nine minutes after launch. The second Centaur stage burn delivered the satellite to a 166 km x 46,076 km x 19.7 deg super-synchronous transfer orbit. The satellite was stationed at 7 deg E and carried 24 Ku-band transponders with a wide beam covering Europe, North Africa and Asia, and a spot beam for digital TV to Turkey. Positioned in geosynchronous orbit at 7 deg E in 1999. As of 26 August 2001 located at 7.01 deg E drifting at 0.004 deg W per day. As of 2007 Mar 7 located at 21.59E drifting at 0.003E degrees per day.

  • 2000 May 24 - Eutelsat W4.  Spacecraft: Spacebus 3000. Mass: 3,190 kg (7,030 lb). Launch Site: Cape Canaveral. Launch Vehicle: Atlas IIIA.

    Communications satellite. Maiden flight of Atlas IIIA with Russian RD-180 main engine; scrubbed four times. European Telecommunications Satellite Organization (Eutelsat) satellite equipped with 32 Ku-band transponders, and antennae covering Russia and Africa. It will be stationed at 36 deg E. This was the third of the high power Eutelsat W series to be launched (W1 was destroyed in a ground accident). Stationed at 36 deg E. Positioned in geosynchronous orbit at 32 deg E in 2000. As of 4 September 2001 located at 35.98 deg E drifting at 0.003 deg E per day. As of 2007 Mar 9 located at 36.08E drifting at 0.005E degrees per day.

  • 2000 September 6 - Eutelsat W1.  Spacecraft: Eurostar 2000. Mass: 3,250 kg (7,160 lb). Launch Site: Kourou. Launch Vehicle: Ariane 44P.

    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.

  • 2001 September 25 - Atlantic Bird 2.  Spacecraft: Spacebus 3000. Mass: 3,149 kg (6,942 lb). Launch Site: Kourou. Launch Vehicle: Ariane 44P.

    Ariane V144 placed the Atlantic Bird 2 satellite in geostationary transfer orbit. Atlantic Bird 2 was an Alcatel/Cannes Spacebus 3000B2 Ku-band communications satellite owned by the European consortium Eutelsat. It replaced the Telecom 2A satellite at 8 deg W. AB-2 had a dry mass of 1368 kg and a launch mass of 3150 kg. Atlantic Bird 1, built by Alenia, was to be launched at a later date. The spacecraft was the twenty-second member of the fleet. and was to provide high-speed television, video streaming, radio and internet services between North and South America, and Europe, North Africa, and the Middle East, through its 26 Ku-band transponders. As of 2007 Mar 9 located at 8.04W drifting at 0.002W degrees per day.

  • 2002 August 21 - Hot Bird 6.  Spacecraft: Spacebus 3000. Mass: 3,905 kg (8,609 lb). Launch Site: Cape Canaveral. Launch Vehicle: Atlas V.

    This was the maiden flight of the Atlas 5 EELV. Launch delayed from May 9, July 8 and 29, August 6 and 12 due to both payload and booster delays. Hot Bird 6 was a European (EUTELSAT) geostationary communications spacecraft. The 4.9-ton Hot Bird 6 (a Spacebus 3000B3) was to provide digital radio and television coverage to Europe, North Africa, and the Middle East through its 28 Ku-band and four Ka-band transponders after being parked over 13° E longitude. As of 2007 Mar 4 located at 12.95E drifting at 0.012E degrees per day.

  • 2002 August 28 - Atlantic Bird 1.  Spacecraft: Italsat. Mass: 2,700 kg (5,900 lb). Launch Site: Kourou. Launch Vehicle: Ariane 5G.

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

  • 2002 November 20 - Eutelsat W5.  Spacecraft: Spacebus 3000. Mass: 3,170 kg (6,980 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta IV Medium.

    Maiden flight of the Delta 4 EELV booster, delayed due to development problems from January and November 2001, April 30, July 15, August 31, October 9, November 3, 16 and 19. EUTELSAT W5 was a European (EUTELSAT Consortium) geostationary communication spacecraft. EUTELSAT W5 was to provide voice, video, and Internet services to all countries in western Europe, central Asia, and the Indian subcontinent through its 24 Ku-band transponders after being parked over 70.5° E longitude. As of 2007 Mar 10 located at 70.55E drifting at 0.004W degrees per day.

  • 2002 December 11 - Hot Bird 7.  Spacecraft: Eurostar 2000. Mass: 3,350 kg (7,380 lb). Launch Site: Kourou. Launch Vehicle: Ariane 5 EC-A.

    Maiden flight of Ariane 5 EC-A. Delayed from October, November 20 and 28. Hot Bird 7, a Eutelsat geostationary communications satellite, was lost in the failed first flight of the Ariane 5 EC-A. Value of the lost satellite was Euro 250 million.

  • 2002 December 11 - Stentor.  Spacecraft: Spacebus 3000. Mass: 2,210 kg (4,870 lb). Launch Site: Kourou. Launch Vehicle: Ariane 5 EC-A.

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

  • 2004 March 15 - W3A.  Spacecraft: Spacebus 3000. Mass: 4,250 kg (9,360 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82M.

    Moved from Ariane 5. The satellite was to provide a full range of telecommunications applications including digital DVB broadcasting, multimedia, broadband access and pay-per-use bandwidth for corporate networks over a large zone covering Europe and Africa, for a minimum of 12 years. As of 2007 Mar 10 located at 6.95E drifting at 0.006W degrees per day.

  • 2006 March 11 - Hot Bird 7A.  Spacecraft: Spacebus 3000. Mass: 4,100 kg (9,000 lb). Launch Site: Kourou. Launch Vehicle: Ariane 5 EC-A.

    Hot Bird 7A had a dry mass of 1740 kg and a solar panel span of 36.9m. As of 2007 Mar 9 located at 13.03E drifting at 0.010E degrees per day.

  • 2006 August 4 - Hot Bird 8.  Spacecraft: Eurostar 3000. Mass: 4,875 kg (10,747 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82M.

    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.

 
 
 
 
 
 
 
 
 

Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2007 except where otherwise noted.

 
Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z