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CHINASAT 6A

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CHINASAT 6A is classified as:


NORAD ID: 37150
Int'l Code: 2010-042A
Perigee: 35,787.3 km
Apogee: 35,802.6 km
Inclination: 0.0 °
Period: 1,436.2 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   21267.85044832 -.00000359  00000-0  00000-0 0  9993
2 37150   0.0353 244.8201 0001816 267.9503 282.3643  1.00267420 40596
Source of the keplerian elements: AFSPC