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JCSAT 2

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JCSAT 2 is classified as:


NORAD ID: 20402
Int'l Code: 1990-001B
Perigee: 36,053.2 km
Apogee: 36,521.3 km
Inclination: 15.4 °
Period: 1,461.4 minutes
Semi major axis: 42658 km
RCS: 1 m2 (large)
Launch date: January 1, 1990
Source: Japan (JPN)
Launch site: AIR FORCE EASTERN TEST RANGE (AFETR)
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 20402U 90001B   24200.50944475  .00000005  00000-0  00000-0 0  9999
2 20402  15.4315  16.7547 0054865 308.1665  47.0942  0.98536856108449
Source of the keplerian elements: AFSPC