Eutelsat 21B

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Eutelsat 21B
NamesEutelsat W6A (pre-launch)
Eutelsat 21B (2012–present)
Mission typeCommunication
OperatorEutelsat
COSPAR ID2012-062B Edit this at Wikidata
SATCAT no.38992
Websitewww.eutelsat.com/en/satellites/the-fleet/EUTELSAT-21B.html
Mission duration15 years
Spacecraft properties
Spacebus 4000C3
ManufacturerThales Alenia Space
Launch mass5,012 kilograms (11,050 lb)
Start of mission
Launch date10 November 2012, 21:05:07 (2012-11-10UTC21:05:07Z) UTC
RocketAriane 5ECA
Launch siteKourou ELA-3
ContractorArianespace
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Longitude21.5° East (2012–present)
Transponders
Band40 Ku-band
 

Eutelsat 21B, previously known as Eutelsat W6A, is a French

direct to home broadcasting services from geostationary orbit at a longitude of 21.5 degrees east. It replaced the Eutelsat 21A
spacecraft which was launched in 1999.

Eutelsat 21B was constructed by

Spacebus-4000C3 satellite bus. It had a mass at launch of 5,012 kilograms (11,050 lb) and is expected to operate for at least 15 years. The satellite carries 40 Ku-band transponders,[1] which are used to broadcast satellite television and radio to Europe, North Africa, Central Asia and the Middle East.[2]

Eutelsat 21B was originally ordered as Eutelsat W6A, as part of the

apogee motor
.

References

  1. ^ Krebs, Gunter. "Eutelsat 21B (Eutelsat W6A)". Gunter's Space Page. Retrieved 5 October 2013.
  2. ^ "EUTELSAT 21B satellite". The Fleet. Eutelsat. Retrieved 5 October 2013.
  3. ^ "TWO TELECOMMUNICATIONS SATELLITES READY FOR LAUNCH" (PDF). Arianespace. Archived from the original (PDF) on 12 October 2013. Retrieved 5 October 2013.
  4. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 5 October 2013.

External links

  • IMS Official provider's site