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JCSAT 2

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JCSAT 2 is classified as:


NORAD ID: 20402
Int'l Code: 1990-001B
Perigee: 36,022.3 km
Apogee: 36,552.7 km
Inclination: 13.6 °
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   18229.00954728 -.00000009  00000-0  00000+0 0  9994
2 20402  13.5668  35.1548 0062175 251.3527 118.0904  0.98535963 87120
Source of the keplerian elements: AFSPC