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Arabsat-1A

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Arabsat-1A () was a Saudi Arabian communications satellite which was operated by Arab Satellite Communications Organization. It was used to provide communication services to the Arab States. It was constructed by Aérospatiale, based on the Spacebus 100 satellite bus, and carries two NATO E/F-band (IEEE S band) and 25 NATO G/H-Band (IEEE C band) transponders. At launch, it had a mass of , and an expected operational lifespan of seven years.

Wikidata facts

Country of origin
France
Followed by
Arabsat-1B
Mass
532
Significant event
breakdown
Show 6 more facts
UTC date of spacecraft launch
1985-02-08
space launch vehicle
Ariane 3
service retirement
1992-03-00
type of orbit
geostationary orbit
service life
7.1
Sources (4)

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Encyclopedic overview

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Arabsat-1A () was a Saudi Arabian communications satellite which was operated by Arab Satellite Communications Organization. It was used to provide communication services to the Arab States. It was constructed by Aérospatiale, based on the Spacebus 100 satellite bus, and carries two NATO E/F-band (IEEE S band) and 25 NATO G/H-Band (IEEE C band) transponders. At launch, it had a mass of , and an expected operational lifespan of seven years.

Arabsat-1A was launched by Arianespace using an Ariane 3 rocket flying from ELA-1 at Kourou. The launch took place at 23:22:00 UTC on 8 February 1985. It was the first Spacebus satellite to be launched. Immediately after launch, one of its solar panels failed to deploy, resulting in reduced performance. It was placed into a geosynchronous orbit at a longitude of 19.0° East. Following a series of gyroscope malfunctions, it was retired from active service, and remained operational as a backup. In September 1991, another problem developed with the spacecraft's attitude control system, and it began to drift eastward. It failed completely in March 1992.

Excerpted from Wikipedia’s “Arabsat-1A” article, available under the CC BY-SA 4.0 licence.

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