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EKRAN 14

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EKRAN 14 is classified as:


NORAD ID: 15626
Int'l Code: 1985-024A
Perigee: 37,297.2 km
Apogee: 37,506.7 km
Inclination: 16.1 °
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   19053.89710698 -.00000105  00000-0  00000+0 0  9991
2 15626  16.1445 342.3914 0023927 310.7053 242.3484  0.94796948 96942
Source of the keplerian elements: AFSPC