Names | Nilesat 104B |
---|---|
Mission type | Communications |
Operator | Eutelsat |
COSPAR ID | 2015-039B![]() |
SATCATno. | 40875 |
Website | www |
Mission duration | 15 years (planned) 9 years, 8 months, 18 days (elapsed) |
Spacecraft properties | |
Spacecraft | Eutelsat 8 West B |
Spacecraft type | Spacebus |
Bus | Spacebus-4000C3 |
Manufacturer | Thales Alenia Space |
Launch mass | 5,782 kg (12,747 lb) |
Power | watts |
Start of mission | |
Launch date | 20 August 2015, 20:34:08UTC |
Rocket | Ariane 5ECA (VA255) |
Launch site | Centre Spatial Guyanais,ELA-3 |
Contractor | Arianespace |
Entered service | October 2015 |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 8° West |
Transponders | |
Band | 50transponders: 10C-band 40Ku-band |
Coverage area | South America, Africa, Middle East |
Eutelsat 8 West B is ageostationarycommunications satellite. Operated byEutelsat, it providesdirect-to-home (DTH) broadcasting services fromgeostationary orbit. The satellite is part of Eutelsat's constellation at alongitude of 8° West. Eutelsat announced the order of a newSpacebus-4000C3satellite bus fromThales Alenia Space in October 2012.
Eutelsat 8 West B is a 5,782 kg (12,747 lb) satellite with a design life of 15 years. It is equipped with anS400-12apogee motor which was used for initialorbit-raising manoeuvres and anS10-18 engine for station keeping burns.[1] The spacecraft has 10C-band and 40Ku-bandtransponders.[2]
Eutelsat 8 West B was launched on theAriane 5ECA launch vehicles fromCentre Spatial Guyanais at theKourou inFrench Guiana. Liftoff occurred at 20:34:08UTC on 20 August 2015,[3] with the launch vehicle successfully injecting its payload intogeosynchronous transfer orbit (GTO). The launch was conducted byArianespace.
Following launch, the satelliteEutelsat 8 West B used its apogee motor to raise itself into geostationary orbit, positioning itself at a longitude of 8° West. Capacity leased byNilesat is marketed asNilesat 104B.[2]