YAMAL 402

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YAMAL 402 is classified as:

Geostationary

NORAD ID: 39022

Int'l Code: 2012-070A

Perigee: 35,778.4 km

Apogee: 35,808.8 km

Inclination: 0.3 °

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.

1 39022U 12070A   25171.44194439  .00000097  00000-0  00000+0 0  9995
2 39022   0.3352  90.0121 0003599 359.3990  33.4858  1.00272385 45972

Source of the keplerian elements: AFSPC