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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,780.5 km
Apogee: 35,989.1 km
Inclination: 11.8 °
Period: 1,440.8 minutes
Semi major axis: 42255 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   20216.06640196 -.00000223  00000-0  00000+0 0  9994
2 13056  11.8012 317.5272 0024691 286.4486  71.2749  0.99947857 97179
Source of the keplerian elements: AFSPC