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EKRAN 14

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EKRAN 14 is classified as:


NORAD ID: 15626
Int'l Code: 1985-024A
Perigee: 37,312.3 km
Apogee: 37,491.6 km
Inclination: 16.0 °
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   19198.90436734 -.00000096 +00000-0 +00000-0 0  9999
2 15626 015.9760 341.0014 0020481 313.1286 048.3492 00.94796949098332
Source of the keplerian elements: AFSPC