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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,784.7 km
Apogee: 35,989.5 km
Inclination: 11.3 °
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   21108.77381875  .00000098  00000-0  00000-0 0  9999
2 13056  11.2857 314.6650 0024230 298.0509 260.3084  0.99939681 99779
Source of the keplerian elements: AFSPC