YAMAL 402

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YAMAL 402 is classified as:

Geostationary

NORAD ID: 39022

Int'l Code: 2012-070A

Perigee: 35,781.5 km

Apogee: 35,806.6 km

Inclination: 0.0 °

Period: 1,436.1 minutes

Semi major axis: 42165 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.

1 39022U 12070A   19321.84235528 +.00000092 +00000-0 +00000-0 0  9990
2 39022 000.0183 313.0586 0002974 296.3059 165.4122 01.00270805025294

Source of the keplerian elements: AFSPC