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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,774.3 km
Apogee: 36,003.0 km
Inclination: 13.2 °
Period: 1,440.9 minutes
Semi major axis: 42259 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   18144.61240927 +.00000076 +00000-0 +00000-0 0  9996
2 13056 013.1895 326.6437 0027066 266.4755 091.3076 00.99934237089178
Source of the keplerian elements: AFSPC