Names | Affordable Modular Optimized Satellite-1 Intelsat 24 IS-24 |
---|---|
Mission type | Communications |
Operator | Spacecom Satellite Communications (1996–2009) Intelsat (2009–2012) |
COSPAR ID | 1996-030B |
SATCAT no. | 23865 |
Website | https://www.amos-spacecom.com/satellites/ |
Mission duration | 12 years (planned) 16 years (achieved) |
Spacecraft properties | |
Spacecraft | AMOS-1 |
Bus | AMOS Bus |
Manufacturer | Israel Aerospace Industries |
Launch mass | 961 kg (2,119 lb) |
Dry mass | 580 kg (1,280 lb) |
Dimensions | 2.33 m × 2.39 m × 2.07 m (7 ft 8 in × 7 ft 10 in × 6 ft 9 in) Span: 10.55 m (34.6 ft) on orbit |
Power | 1380 watts |
Start of mission | |
Launch date | 16 May 1996, 01:56:29 UTC |
Rocket | Ariane 44L H10-3 (V86) |
Launch site | Centre Spatial Guyanais, Kourou, ELA-2 |
Contractor | Arianespace |
Entered service | 1 July 1996 |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | July 2012 |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 4° West (1996–2008) 47.3° East (2009–2011) 31° East (2011–2012) |
Transponders | |
Band | 7 (+ 2 spares) Ku-band |
Bandwidth | 72 MHz |
Coverage area | Europe, Israel, Middle East |
AMOS-1, then Intelsat 24, was a commercial communications satellite which was operated by Spacecom as AMOS-1, for Affordable Modular Optimized Satellite and formed part of the AMOS series of satellites. It was the first Israeli civilian communications satellite, and was initially positioned at 4° West longitude in geostationary orbit.[1] Then in September 2011, it was moved to 31° East.[2]