Intelsat V F-2

Intelsat V F-2 → Intelsat 502
Mission type Communication
Operator Intelsat
COSPAR ID 1980-098A[1]
SATCAT no. 12089[1]
Mission duration 18 years
Spacecraft properties
Bus Intelsat-V bus
Manufacturer Ford Aerospace
Launch mass 1,928.2 kilograms (4,251 lb)
BOL mass 1,012 kilograms (2,231 lb)
Start of mission
Launch date 06 December 1980, 23:31 (1980-12-06UTC23:31Z) UTC
Rocket Atlas SLV-3D Centaur-D1AR
Launch site Cape Canaveral LC-36B
End of mission
Disposal Decommissioned
Deactivated April 14, 1998 (1998-04-15)
Orbital parameters
Reference system Geocentric
Regime Geostationary
Eccentricity 0.72568
Perigee 169 kilometres (105 mi)
Apogee 34,834 kilometres (21,645 mi)
Inclination 0 degrees
Period 614.9 minutes
Epoch December 06, 1980
Transponders
Band 21 C-band
4 Ku band
Intelsat V

Intelsat 502, previously named Intelsat V F-2, was a communications satellite operated by Intelsat. Launched in 1980, it was the second of fifteen Intelsat VI 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. The satellite was deactivated on April 14, 1998.

The satellite was successfully launched into space on December 6, 1980, at 23:31 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 1,928 kg. The Intelsat 502 was equipped with 4 Ku-band transponders more 21 C-band transponders for 12,000 audio circuits and 2 TV channels.

References

  1. 1 2 "INTELSAT 5 F-2". National Space Science Data Center. Retrieved April 22, 2017.


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