Names | ECS-1 European Communications Satellite-1 Eutelsat 1 |
---|---|
Mission type | Communications |
Operator | ESA / Eutelsat |
COSPAR ID | 1983-058A |
SATCAT no. | 14128 |
Website | https://www.eutelsat.com/en/home.html |
Mission duration | 7 years (planned) 13 years (achieved) |
Spacecraft properties | |
Spacecraft | ECS-1 |
Spacecraft type | ECS |
Bus | ECS-Bus |
Manufacturer | British Aerospace |
Launch mass | 1,158 kg (2,553 lb) [1] |
Dry mass | 500 kg (1,100 lb) |
Dimensions | 1.9 m x 1.4 m x 2.3 m Span on orbit: 13.8 m |
Power | 1 kW |
Start of mission | |
Launch date | 16 June 1983, 11:59:03 UTC[2] |
Rocket | Ariane 1 (L06) |
Launch site | Centre Spatial Guyanais, ELA-1 |
Contractor | Arianespace |
Entered service | 12 October 1983 |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | 16 December 1996 |
Orbital parameters | |
Reference system | Geocentric orbit[3] |
Regime | Geostationary orbit |
Longitude | 13° East (1983–1988) 16° East (1988–1991) 17.5° East (1991–1992) 25.5° East (1992–1993) 48° East (1993–1996) 36° East (1996) [4] |
Transponders | |
Band | 12 Ku-band |
Bandwidth | 72 MHz |
Coverage area | Europe, the Middle East and Africa |
Eutelsat I F-1, also known as European Communications Satellite 1 (ECS-1) is a decommissioned communications satellite operated by the European Telecommunications Satellite Organisation (Eutelsat). Launched in 1983, it was operated in geostationary orbit at a longitude of 13° East, before moving to several other locations later in its operational life, before it was finally decommissioned in 1996. It was the first of five satellites launched to form the first-generation Eutelsat constellation.
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