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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: 35,994.5 km
Inclination: 8.9 °
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   24115.84814965 -.00000278  00000-0  00000-0 0  9990
2 13056   8.8686 303.2565 0026121 322.3455  40.2318  0.99950208110791
Source of the keplerian elements: AFSPC