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XM-5

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XM-5 is classified as:


NORAD ID: 37185
Int'l Code: 2010-053A
Perigee: 35,789.6 km
Apogee: 35,797.5 km
Inclination: 0.0 °
Period: 1,436.1 minutes
Semi major axis: 42164 km
RCS: 2 m2 (large)
Launch date: October 14, 2010
Source: United States (US)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

The satellite will be an orbital spare for the XM 3 and XM 4 satellites currently transmitting operational radio signals. Sirius XM 5 will join a fleet of spacecraft already beaming radio signals to receivers in cars, trucks, boats, aircraft, homes and mobile devices of more than 19.8 million subscribers. Two 29.5-foot-diameter (9-m-diameter) unfurlable mesh antennas will broadcast Sirius XM Radio's 135 audio channels. The antennas will be connected to an S-band downlink and X-band uplink communications payload. The satellite is designed to last for at least 15 years in space. Based on Loral's 1300 spacecraft bus, Sirius XM 5 will produce nearly 20 kilowatts of power at the end of its mission.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 37185U 10053A   17325.15375793 -.00000201  00000-0  00000+0 0  9994
2 37185   0.0113 293.8247 0000946  98.0373 358.6554  1.00272458 26064
Source of the keplerian elements: AFSPC