AMOS-1 (satellite)

AMOS-1
NamesAffordable Modular Optimized Satellite-1
Intelsat 24
IS-24
Mission typeCommunications
OperatorSpacecom Satellite Communications (1996–2009)
Intelsat (2009–2012)
COSPAR ID1996-030B Edit this at Wikidata
SATCAT no.23865
Websitehttps://www.amos-spacecom.com/satellites/
Mission duration12 years (planned)
16 years (achieved)
Spacecraft properties
SpacecraftAMOS-1
BusAMOS Bus
ManufacturerIsrael Aerospace Industries
Launch mass961 kg (2,119 lb)
Dry mass580 kg (1,280 lb)
Dimensions2.33 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
Power1380 watts
Start of mission
Launch date16 May 1996, 01:56:29 UTC
RocketAriane 44L H10-3 (V86)
Launch siteCentre Spatial Guyanais, Kourou, ELA-2
ContractorArianespace
Entered service1 July 1996
End of mission
DisposalGraveyard orbit
DeactivatedJuly 2012
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Longitude4° West (1996–2008)
47.3° East (2009–2011)
31° East (2011–2012)
Transponders
Band7 (+ 2 spares) Ku-band
Bandwidth72 MHz
Coverage areaEurope, Israel, Middle East
AMOS-2 →

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]

  1. ^ Jameson, Helen. "Tackling the Challenges of Communication" (PDF). Global Military Communications. Archived from the original (PDF) on 17 September 2012. Retrieved 14 June 2012.
  2. ^ "AMOS 1". The Satellite Encyclopedia. 28 February 2021. Retrieved 6 May 2021.