Intelsat V F-3

Intelsat V F-3 → Intelsat 503
Mission type Communication
Operator Intelsat
COSPAR ID 1981-119A[1]
SATCAT no. 12994[1]
Mission duration 17 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 December 15, 1981, 23:35 (1981-12-15UTC23:35Z) UTC
Rocket Atlas SLV-3D Centaur-D1AR
Launch site Cape Canaveral LC-36B
End of mission
Disposal Decommissioned
Deactivated January 1998 (1998-02)
Orbital parameters
Reference system Geocentric
Regime Geostationary
Eccentricity 0.73207
Perigee 165 kilometres (103 mi)
Apogee 35,947 kilometres (22,336 mi)
Inclination 23.7 degrees
Period 633.5 minutes
Epoch December 15, 1981
Transponders
Band 21 C-band
4 Ku band
Intelsat V
Launch of Intelsat V F-3.

Intelsat 503, previously named Intelsat V F-3, was a communications satellite operated by Intelsat. Launched in 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-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 January 1998.

The satellite was successfully launched into space on December 15, 1981, at 23:35 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 503 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-3". National Space Science Data Center. Retrieved April 22, 2017.


This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.