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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,771.1 km
Apogee: 36,003.1 km
Inclination: 9.0 °
Period: 1,440.9 minutes
Semi major axis: 42258 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   24063.42815748  .00000132  00000-0  00000-0 0  9994
2 13056   8.9879 303.7476 0027445 322.1900 258.1400  0.99939596110266
Source of the keplerian elements: AFSPC