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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,780.9 km
Apogee: 35,996.9 km
Inclination: 12.5 °
Period: 1,441.0 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   19176.50591269 -.00000295  00000-0  00000+0 0  9991
2 13056  12.5446 322.1069 0025558 278.0428 321.7338  0.99933195 93139
Source of the keplerian elements: AFSPC