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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,760.9 km
Apogee: 36,009.7 km
Inclination: 12.9 °
Period: 1,440.8 minutes
Semi major axis: 42256 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   18324.76327414 -.00000032 +00000-0 +00000-0 0  9992
2 13056 012.9111 324.5777 0029441 275.1802 100.2179 00.99946228090987
Source of the keplerian elements: AFSPC