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EKRAN 14

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EKRAN 14 is classified as:


NORAD ID: 15626
Int'l Code: 1985-024A
Perigee: 37,337.2 km
Apogee: 37,466.2 km
Inclination: 14.3 °
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   22223.14146538 -.00000139  00000-0  00000-0 0  9996
2 15626  14.3383 331.0723 0014736 335.0331  22.8437  0.94797852108941
Source of the keplerian elements: AFSPC