Mission type | Communications |
---|---|
Operator | COMSAT / INTELSAT |
COSPAR ID | 1981-050A |
SATCAT no. | 12474 |
Mission duration | 7 years (planned) |
Spacecraft properties | |
Bus | Intelsat V |
Manufacturer | Ford Aerospace |
Launch mass | 1928 kg |
Dry mass | 1012 kg |
Dimensions | 1.66 x 2.1 x 1.77 metres |
Power | 1800 watts |
Start of mission | |
Launch date | 23 May 1981, 22:42:00 UTC [1] |
Rocket | Atlas SLV-3D Centaur (AC-56) |
Launch site | CCAFS, LC-36B |
Contractor | General Dynamics |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | February 1997 |
Orbital parameters | |
Reference system | Geocentric orbit [2] |
Regime | Geostationary orbit |
Longitude | 177.0° West (1981-1992) 91.5° East (1992-1996) 72.0° East (1996-1997) |
Epoch | 23 May 1981 |
Transponders | |
Band | 21 C-band 4 Ku-band |
Intelsat V |
Intelsat V F-1 (or Intelsat 501) was a geostationary communications satellite built by Ford Aerospace, it was owned by COMSAT. Launched in 1981, it was the second of fifteen Intelsat V satellites to be launched. The satellite was based on the Intelsat V platform and its estimated useful life was seven years.
The satellite was box-shaped, measuring 1.66 by 2.1 by 1.77 metres; solar arrays spanned 15.9 metres tip to tip. The arrays, supplemented by nickel-hydrogen batteries during eclipse, provided 1800 watts of power. The payload housed 21 C-band and 4 Ku-band transponders. It could accommodate 15,000 two-way voice circuits and two TV channels simultaneously. It had a launch mass of 1928 kg. [3] The satellite was deactivated in February 1997.
The satellite was successfully launched into space on 23 May 1981, at 22:42:00 UTC, by means of an Atlas SLV-3D Centaur vehicle from the CCAFS, LC-36B. [4]
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