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JCSAT 2

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JCSAT 2 is classified as:


NORAD ID: 20402
Int'l Code: 1990-001B
Perigee: 36,032.3 km
Apogee: 36,540.5 km
Inclination: 14.7 °
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   22025.79949431 -.00000234  00000-0  00000-0 0  9995
2 20402  14.7212  24.0046 0059565 287.8585 242.0887  0.98539778 99539
Source of the keplerian elements: AFSPC