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JCSAT 2

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JCSAT 2 is classified as:


NORAD ID: 20402
Int'l Code: 1990-001B
Perigee: 36,009.8 km
Apogee: 36,563.0 km
Inclination: 13.8 °
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   19048.70921490 -.00000198 +00000-0 +00000-0 0  9991
2 20402 013.7627 033.3838 0064841 259.7518 111.8715 00.98539582088968
Source of the keplerian elements: AFSPC