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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,769.5 km
Apogee: 36,000.0 km
Inclination: 12.1 °
Period: 1,440.7 minutes
Semi major axis: 42255 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   20047.49146410 -.00000021 +00000-0 +00000-0 0  9990
2 13056 012.1199 319.4259 0027282 290.7278 253.7913 00.99948017095505
Source of the keplerian elements: AFSPC