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EKRAN 14

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EKRAN 14 is classified as:


NORAD ID: 15626
Int'l Code: 1985-024A
Perigee: 37,317.5 km
Apogee: 37,486.3 km
Inclination: 15.1 °
Period: 1,519.0 minutes
Semi major axis: 43772 km
RCS: 10.1631 m2 (large)
Launch date: March 22, 1985
Source: Commonwealth of Independent States (former USSR) (CIS)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 15626U 85024A   21108.82410807 -.00000092  00000-0  00000-0 0  9993
2 15626  15.0978 335.1236 0019280 336.5942 239.0708  0.94797021104404
Source of the keplerian elements: AFSPC