Mission type | Communication |
---|---|
Operator | COMSAT / INTELSAT |
COSPAR ID | 1983-047A [1] |
SATCAT no. | 14077 |
Mission duration | 7 years (planned) |
Spacecraft properties | |
Bus | Intelsat V |
Manufacturer | Ford Aerospace |
Launch mass | 1928 kg |
Dry mass | 1012 kg [2] |
Dimensions | 1.66 x 2.1 x 1.77 metres |
Power | 1800 watts |
Start of mission | |
Launch date | 19 May 1983, 22:26:00 UTC [3] |
Rocket | Atlas SLV-3D Centaur-D1AR (AC-61) |
Launch site | CCAFS, LC-36A |
Contractor | General Dynamics |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | July 1998 |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 18,5° West (1983-1992) 50.0° West (1992-1995) 31.4° West (1995-1998) 29.5° West (1998-1998) |
Epoch | 19 May 1983 |
Transponders | |
Band | 21 C-band 4 Ku-band |
Intelsat V |
Intelsat V F-6, then named Intelsat 506, was a communications satellite operated by COMSAT. Launched in 1983, it was the sixth of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat V satellite bus. Intelsat V F-6 was part of an advanced series of satellites designed to provide greater telecommunications capacity for INTELSAT's global network.
The Intelsat V F-6 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. He also carried a Maritime Communications Services (MCS) package for INMARSAT. [4] The satellite was deactivated in July 1998.
The satellite was successfully launched into space on 19 May 1982 at 22:26:00 UTC, by means of an Atlas SLV-3D Centaur-D1AR vehicle from the Cape Canaveral Air Force Station, Florida, United States. It had a launch mass of 1928 kg. [5]
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Intelsat IV F-5 was a geostationary communication satellite built by Hughes, it was owned by Intelsat. The satellite was based on the HS-312 platform and its estimated useful life was 7 years.
Intelsat IV F-6 was a geostationary communication satellite built by Hughes, it was owned by Intelsat. The satellite was based on the HS-312 platform and its estimated useful life was 7 years.
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Intelsat V F-2, then named Intelsat 502, was a communications satellite operated by COMSAT. Launched in 1980, it was the first of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat V satellite bus. Intelsat V F-2 was part of an advanced series of satellites designed to provide greater telecommunications capacity for INTELSAT's global network.
Intelsat V F-3, then named Intelsat 503, was a communications satellite operated by COMSAT. Launched on 15 December 1981, it was the third of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat V satellite bus. Intelsat V F-3 was part of an advanced series of satellites designed to provide greater telecommunications capacity for Intelsat's global network.
Intelsat V F-4, then named Intelsat 504, was a communications satellite operated by COMSAT. Launched in 1982, it was the fourth of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat V satellite bus. Intelsat V F-4 was part of an advanced series of satellites designed to provide greater telecommunications capacity for Intelsat's global network.
Intelsat V F-5, then named Intelsat 505, was a communications satellite operated by COMSAT. Launched in 1982, it was the fifth of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat V satellite bus. Intelsat V F-5 was part of an advanced series of satellites designed to provide greater telecommunications capacity for Intelsat's global network.
Intelsat 507, previously named Intelsat V F-7, was a communications satellite operated by Intelsat. Launched in 1983, it was the seventh of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat-V satellite bus. It was the first satellite of the Intelsat family not to be launched by the United States.
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Intelsat VA F-13 or Intelsat 513, then named 'NSS-513', was a communications satellite operated by Intelsat and which was later sold to New Satellite Skies. Launched in 1988, it was the thirteenth of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat VA satellite bus. Intelsat VA F-13 was part of an advanced series of satellites designed to provide greater telecommunications capacity for Intelsat's global network.
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Intelsat VA F-15 or Intelsat 515, then named Columbia 515, was a communications satellite operated by Intelsat and which was later sold to Columbia Communications Corporation. Launched in 1989, it was the fifteenth of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat VA satellite bus. Intelsat VA F-15 was part of an advanced series of satellites designed to provide greater telecommunications capacity for Intelsat's global network, from an orbital station at 60.0° East.
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