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JCSAT 2

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JCSAT 2 is classified as:


NORAD ID: 20402
Int'l Code: 1990-001B
Perigee: 36,045.7 km
Apogee: 36,527.8 km
Inclination: 15.4 °
Period: 1,461.4 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   24134.08313174 -.00000172  00000-0  00000-0 0  9990
2 20402  15.3823  17.2892 0056504 307.9979 242.5570  0.98538621107796
Source of the keplerian elements: AFSPC