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JCSAT 2

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JCSAT 2 is classified as:


NORAD ID: 20402
Int'l Code: 1990-001B
Perigee: 36,028.3 km
Apogee: 36,544.4 km
Inclination: 13.9 °
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   19198.84539587 -.00000256 +00000-0 +00000-0 0  9999
2 20402 013.9116 031.9815 0060498 263.1981 089.2835 00.98539901090430
Source of the keplerian elements: AFSPC