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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,773.8 km
Apogee: 36,002.8 km
Inclination: 12.7 °
Period: 1,440.9 minutes
Semi major axis: 42259 km
RCS: 6.2092 m2 (large)
Launch date: February 5, 1982
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 13056U 82009A   19082.33555928 +.00000087 +00000-0 +00000-0 0  9999
2 13056 012.7060 323.1754 0027092 281.2697 274.5408 00.99935450092198
Source of the keplerian elements: AFSPC