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JCSAT 2

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JCSAT 2 is classified as:


NORAD ID: 20402
Int'l Code: 1990-001B
Perigee: 36,028.6 km
Apogee: 36,545.9 km
Inclination: 13.9 °
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   19235.41100603 -.00000052 +00000-0 +00000-0 0  9991
2 20402 013.9465 031.6389 0060637 263.2347 100.8934 00.98536848090800
Source of the keplerian elements: AFSPC