Intelsat III F-2

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Intelsat III F-2
Mission typeCommunications
OperatorCOMSAT for Intelsat
COSPAR ID1968-116A Edit this at Wikidata
SATCAT no.03623
Mission duration5 years (planned)
1+12 years (achieved)
Spacecraft properties
Spacecraft typeIntelsat III
BusIntelsat
ManufacturerTRW
Launch mass293 kg
Dry mass151 kg
Power183 watts
Start of mission
Launch date19 December 1968,
00:32:00
Cape Canaveral, LC-17A
ContractorNASA
End of mission
DeactivatedMid-1971
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
(Now supersynchronous)
Longitude24.0° West
Transponders
Capacity2 transponders
Coverage areaGlobal
 

Intelsat III F-2 was a communications satellite operated by Intelsat. Launched in 1968 it was operated in geostationary orbit at a longitude of 24 degrees west for around eighteen months.[2]

Spacecraft

The second of eight

apogee motor for propulsion and was equipped with two transponders powered by body-mounted solar cells generating 183 watts of power.[2] It was designed for a five-year service life.[3]

Launch

The launch of Intelsat III F-2 made use of a

geosynchronous transfer orbit.[1] Intelsat III F-2 subsequently fired its apogee motor to achieve geostationary orbit. It was operated at a longitude of 24° west, over Brazil; however it ceased operations after only a year and a half in orbit, in mid-1971.[4]

Orbit

Intelsat III F-2 remains in a

orbital debris. As of 7 February 2014, it was in an orbit with a perigee of 38,438 km (23,884 mi), an apogee of 39,317 km (24,430 mi), inclination of 13.73° and an orbital period of 26.60 hours.[5]

See also

References

  1. ^ a b McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 9 February 2014.
  2. ^ a b Wade, Mark. "Intelsat 3". Encyclopedia Astronautica. Archived from the original on 23 February 2002. Retrieved 9 February 2014.
  3. ^ Krebs, Gunter. "Intelsat-3". Gunter's Space Page. Retrieved 9 February 2014.
  4. ^ "Intelsat 3 Quicklook". Mission and Spacecraft Library. NASA Jet Propulsion Laboratory. Retrieved 9 February 2014. Public Domain This article incorporates text from this source, which is in the public domain.
  5. ^ "INTELSAT 3-F2 Satellite details 1968-116A NORAD 3623". N2YO. 7 February 2014. Retrieved 9 February 2014.