Star One C3

Last updated
Star One C3
Mission type Communication
Operator Star One
COSPAR ID 2012-062A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 38991
Mission duration15 years (planned)
Spacecraft properties
Bus STAR-2
Manufacturer Orbital Sciences Corporation
Launch mass3,227 kilograms (7,114 lb)
Start of mission
Launch date10 November 2012, 21:05 (2012-11-10UTC21:05Z) UTC
Rocket Ariane 5ECA
Launch site Kourou ELA-3
Contractor Arianespace
Orbital parameters
Reference system Geocentric
Regime Geostationary
Longitude75° and 84° west
Semi-major axis 42,164.0 kilometres (26,199.5 mi)
Perigee altitude 35,787.6 kilometres (22,237.4 mi)
Apogee altitude 35,799.5 kilometres (22,244.8 mi)
Period 1,436.1 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]

Contents

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

See also

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References

  1. "Arianespace - Mission Update - Ariane 5 is poised for Arianespace's launch with the EUTELSAT 21B and Star One C3 satellites". 2012-11-11. Archived from the original on 2012-11-11. Retrieved 2023-05-20.
  2. "Wayback Machine" (PDF). 2013-12-16. Archived from the original (PDF) on 2013-12-16. Retrieved 2023-05-20.