Intelsat V F-1

Intelsat V F-1 → Intelsat 501
Mission type Communications
Operator Intelsat
COSPAR ID 1981-050A
SATCAT no. 12474
Mission duration 7 years (planned)
Spacecraft properties
Bus Intelsat-V bus
Manufacturer Ford Aerospace
Launch mass 1,928 kilograms (4,251 lb)
BOL mass 1,012 kilograms (2,231 lb)
Power 1800 W
Start of mission
Launch date May 23, 1981, 22:42 (1981-05-23UTC22:42Z) UTC[1]
Rocket Atlas SLV-3D Centaur-D1AR
Launch site Cape Canaveral LC-36B
End of mission
Deactivated February 1997 (1997-03)
Orbital parameters
Reference system Geocentric[2]
Regime Geostationary[2]
Eccentricity 0.73189[2]
Perigee 172 kilometers (107 mi)[2]
Apogee 35,960 kilometers (22,340 mi)[2]
Inclination 24.1°[2]
Period 633.9 minutes[2]
Epoch May 23, 1981[2]
Transponders
Band 21 IEEE C-band
4 Ku band
Intelsat V

Intelsat V F-1 (or Intelsat 501) was a geostationary communication satellite built by Ford Aerospace, it was owned by Intelsat. The satellite was based on the Intelsat-V platform and its estimated useful life was 7 years.

See also

References

  1. McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved April 22, 2017.
  2. 1 2 3 4 5 6 7 8 NASA, Goddard Space Flight Center. "INTELSAT 5 F-1". NSSDC Master Catalog. Retrieved April 22, 2017.
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