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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,778.2 km
Apogee: 36,001.7 km
Inclination: 11.6 °
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   20295.21264002 +.00000004 +00000-0 +00000-0 0  9993
2 13056 011.6495 316.6457 0026439 289.8705 103.6750 00.99929489097982
Source of the keplerian elements: AFSPC