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Star One C3

From Wikipedia, the free encyclopedia

Star One C3
Mission typeCommunication
OperatorStar One
COSPAR ID2012-062A Edit this at Wikidata
SATCAT no.38991
Mission duration15 years (planned)
Spacecraft properties
BusSTAR-2
ManufacturerOrbital Sciences Corporation
Launch mass3,227 kilograms (7,114 lb)
Start of mission
Launch date10 November 2012, 21:05 (2012-11-10UTC21:05Z) UTC
RocketAriane 5ECA
Launch siteKourou ELA-3
ContractorArianespace
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Longitude75° and 84° west
Semi-major axis42,164.0 kilometres (26,199.5 mi)
Perigee altitude35,787.6 kilometres (22,237.4 mi)
Apogee altitude35,799.5 kilometres (22,244.8 mi)
Period1,436.1 minutes
Transponders
Band28 IEEE C-band (NATO G/H-band)
16 IEEE Ku band (NATO J-band)

Star One C3 is a communications satellite operated by Star One, a subsidiary of Embratel. It was built by Orbital Sciences Corporation based on the STAR-2 satellite bus, and was launched on 10 November 2012 21:05 UTC by an Ariane 5ECA carrier rocket, as part of a dual-payload launch with Eutelsat 21B.[1]

Star One C3 will replace Brasilsat B3 in the 75° W position. The launch mass was 3226.6 kg.[2]

See also

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References

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  1. "Arianespace - Mission Update - Ariane 5 is poised for Arianespace's launch with the EUTELSAT 21B and Star One C3 satellites". 11 November 2012. Archived from the original on 11 November 2012. Retrieved 20 May 2023.
  2. Sander, Catherine (November 2012). "Ariane 5 Data Relating to Flight 210" (PDF). Astrium. pp. 24–25. Archived from the original on 16 December 2013. Retrieved 8 August 2023.
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