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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,779.9 km
Apogee: 35,999.7 km
Inclination: 10.7 °
Period: 1,441.0 minutes
Semi major axis: 42260 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   22023.18173698  .00000136  00000-0  00000-0 0  9996
2 13056  10.6999 311.6241 0026003 304.2824 344.2286  0.99929982102563
Source of the keplerian elements: AFSPC