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YAMAL 402

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YAMAL 402 is classified as:


NORAD ID: 39022
Int'l Code: 2012-070A
Perigee: 35,782.4 km
Apogee: 35,804.5 km
Inclination: 0.0 °
Period: 1,436.1 minutes
Semi major axis: 42164 km
RCS: 2.3115 m2 (large)
Launch date: December 8, 2012
Source: Commonwealth of Independent States (former USSR) (CIS)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

YAMAL 402 was supposed to maneuver itself into a circular geosynchronous orbit 22,300 miles (35,888 km) up and lowering inclination where it can match Earth's rotation and appear parked over the equator at 55 degrees East longitude to begin a 15-year service life. However the upper stage of the heavy-lift Proton rocket failed to perform the full duration of its final boost-burn, leaving YAMAL 402 in a lower-than-planned orbit at the end of a 9-hour flight from the Baikonur Cosmodrome.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 39022U 12070A   17108.99755815 +.00000077 +00000-0 +10000-3 0  9990
2 39022 000.0104 185.9569 0002622 214.6557 220.6940 01.00272685016043
Source of the keplerian elements: AFSPC