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JCSAT 2

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JCSAT 2 is classified as:


NORAD ID: 20402
Int'l Code: 1990-001B
Perigee: 36,032.7 km
Apogee: 36,539.9 km
Inclination: 14.5 °
Period: 1,461.3 minutes
Semi major axis: 42657 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   21101.61978869 -.00000251  00000-0  00000-0 0  9996
2 20402  14.4856  26.4018 0059448 283.2421 260.3908  0.98540027 96683
Source of the keplerian elements: AFSPC