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EKRAN 4

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EKRAN 4 is classified as:


NORAD ID: 11561
Int'l Code: 1979-087A
Perigee: 35,788.6 km
Apogee: 35,800.4 km
Inclination: 12.5 °
Period: 1,436.1 minutes
Semi major axis: 42165 km
RCS: 0.1995 m2 (medium)
Launch date: October 3, 1979
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 11561U 79087A   17326.40986774 -.00000291 +00000-0 +00000-0 0  9992
2 11561 012.5314 321.0638 0001407 287.7517 057.6068 01.00269038015999
Source of the keplerian elements: AFSPC