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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,779.4 km
Apogee: 35,994.2 km
Inclination: 12.0 °
Period: 1,440.9 minutes
Semi major axis: 42257 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   20096.50406647 -.00000370 +00000-0 +00000-0 0  9994
2 13056 012.0292 318.8723 0025415 290.7072 249.9644 00.99940876095991
Source of the keplerian elements: AFSPC