Intelsat V F-4

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Intelsat V F-4 → Intelsat 504
Mission typeCommunication
OperatorIntelsat
COSPAR ID1982-017A[1]
SATCAT no.13083[1]
Mission duration13 years
Spacecraft properties
BusIntelsat-V bus
ManufacturerFord Aerospace
Launch mass1,928.2 kilograms (4,251 lb)
BOL mass1,012 kilograms (2,231 lb)
Start of mission
Launch dateMarch 5, 1982, 00:23 (1982-03-05UTC00:23Z) UTC[2]
RocketAtlas SLV-3D Centaur-D1AR
Launch siteCape Canaveral LC-36A
End of mission
DisposalDecommissioned
DeactivatedNovember 1995 (1995-12)
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Eccentricity0.57914
Perigee altitude6,547 kilometres (4,068 mi)
Apogee altitude42,132 kilometres (26,180 mi)
Inclination24.1 degrees
Period629.8 minutes
EpochMarch 5, 1982[1]
Transponders
Band21 C-band
4 Ku band
Intelsat V
 

Intelsat 504, previously named Intelsat V F-4, was a communications satellite operated by Intelsat. 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. The satellite was deactivated on November 1995.

The satellite was successfully launched into space on March 5, 1982, at 00:23 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 504 was equipped with 4 Ku-band transponders more 21 C-band transponders for 12,000 audio circuits and 2 TV channels.

References[edit]

  1. ^ a b c "INTELSAT 5 F-4". National Space Science Data Center. Retrieved April 23, 2017.
  2. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved April 22, 2017.