Sirius FM-5
Mission type | Communication |
---|---|
Operator | Sirius XM Radio |
COSPAR ID | 2009-034A |
SATCAT № | 35493 |
Mission duration | 15 years |
Spacecraft properties | |
Bus | LS-1300 |
Manufacturer | Space Systems Loral |
Launch mass | 5,820 kilograms (12,830 lb) |
Start of mission | |
Launch date | 30 June 2009, 19:10:00 UTC |
Rocket | Proton-M/Briz-M |
Launch site | Baikonur 200/39 |
Contractor | ILS |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 96° west |
Perigee | 35,784 kilometers (22,235 mi) |
Apogee | 35,801 kilometers (22,246 mi) |
Inclination | 0.01 degrees |
Period | 24 hours |
Epoch | January 21, 2014, 08:13:09 UTC[1] |
Transponders | |
Band | 1 E/F/I-band |
Coverage area | North America |
Sirius FM-5, also known as Radiosat 5, is an American communications satellite which will be operated by Sirius XM Radio. It was constructed by Space Systems Loral, based on the LS-1300 bus, and carries a single transponder designed to transmit in the NATO E F and I bands (IEEE S and X bands). It will be used to provide satellite radio broadcasting to North America.
Sirius FM-5 was launched by a Proton-M/Briz-M rocket flying from Site 200/39 at the Baikonur Cosmodrome. The launch was conducted by International Launch Services, and occurred at 19:10 GMT on 30 June 2009. Around nine hours after launch, the satellite separated from the carrier rocket into a geosynchronous transfer orbit. It will raise itself into geostationary orbit by means of its onboard R-4D apogee motor. It also carries four SPT-100 engines for manoeuvring.
It is the first Sirius Radio satellite to be placed in geostationary orbit; the three previous Sirius satellites operate in tundra orbits.
See also
References
- ↑ "SIRIUS FM-5 Satellite details 2009-034A NORAD 35493". N2YO. January 21, 2014. Retrieved January 21, 2014.
- Krebs, Gunter. "Sirius FM5, FM6 (Radiosat 5, 6)". Gunter's Space Page. Retrieved 2009-06-30.
- "Sirius FM-5 Blog". International Launch Services. Retrieved 2009-06-30.
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