Eutelsat I F-1
| 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) |
| 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 |
| 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 |
| 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) |
| 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.