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CHINASAT 6A

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CHINASAT 6A is classified as:


NORAD ID: 37150
Int'l Code: 2010-042A
Perigee: 35,780.8 km
Apogee: 35,807.6 km
Inclination: 0.0 °
Period: 1,436.1 minutes
Semi major axis: 42165 km
RCS: 50.1187 m2 (large)
Launch date: September 4, 2010
Source: People's Republic of China (PRC)
Launch site: Xichang Space Center, China (XSC)

Chinasat 6A is a Chinese communication satellite that will use its own propulsion system to circularize its orbit at an altitude of 22,300 miles (35,900 km) above the equator near Indonesia. The satellite is designed to last 15 years delivering television and radio programming to customers across China, especially in remote and mountainous regions.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 37150U 10042A   19235.60656877 -.00000357 +00000-0 +00000-0 0  9994
2 37150 000.0275 158.4446 0003183 031.8185 124.7473 01.00270136032930
Source of the keplerian elements: AFSPC