EKRAN 8

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EKRAN 8 is classified as:

• Geostationary

NORAD ID: 13056
Int'l Code: 1982-009A
Perigee: 35,777.0 km
Apogee: 35,994.4 km
Inclination: 8.8 °
Period: 1,440.8 minutes
Semi major axis: 42256 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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1 13056U 82009A   24130.62407016 -.00000363  00000-0  00000-0 0  9993
2 13056   8.8348 303.1175 0025720 321.8764 317.4804  0.99944544110934

Source of the keplerian elements: AFSPC