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EKRAN 8

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EKRAN 8 is classified as:


NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,760.3 km
Apogee: 36,021.2 km
Inclination: 13.5 °
Period: 1,441.1 minutes
Semi major axis: 42261 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   17326.53240421 -.00000104  00000-0  00000+0 0  9999
2 13056  13.4554 328.7279 0030864 263.1445 104.8308  0.99926725 87337
Source of the keplerian elements: AFSPC