JCSAT 2

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JCSAT 2 is classified as:

NORAD ID: 20402

Int'l Code: 1990-001B

Perigee: 36,046.9 km

Apogee: 36,527.6 km

Inclination: 15.4 °

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)

Your satellite tracking list

Two Line Element Set (TLE):

1 20402U 90001B   24140.16617390 -.00000025  00000-0  00000+0 0  9999
2 20402  15.3868  17.2414 0056343 308.0295 240.4680  0.98536908107839

Source of the keplerian elements: AFSPC