AYAME 1 DEB

NORAD ID: 38682

Int'l Code: 1979-009E

Perigee: 12,461.1 km

Apogee: 34,448.0 km

Inclination: 10.7 °

Period: 854.4 minutes

Semi major axis: 29825 km

RCS: 0.003 m² (small)

Launch date: February 6, 1979
Source: Japan (JPN)
Launch site: TANEGASHIMA SPACE CENTER (TNSTA)

Note: This is SATELLITE DEBRIS

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Two Line Element Set (TLE):

1 38682U 79009E   24115.34355464 -.00000137  00000-0  00000-0 0  9991
2 38682  10.7154 344.2825 3685911  53.3787 335.2190  1.68546610 72493

Source of the keplerian elements: AFSPC