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SOCRATES
Launch Details
Launched | 23 May 2014 |
Flight ended | – |
Status | Operational |
Category |
Active satellites
|
Launch site | Tanegashima Space Center, Japan |
Owner | Japan |
NORAD ID | 39768 |
COSPAR ID | 2014-029C |
Observing |
Current orbital elements
Inclination | 97.888° |
Eccentricity | 0.00076 |
RA ascending node | 19.224 hr |
Argument perigee | 71.615° |
Mean anomaly | 288.590° |
Orbital period | 96.465 min |
Epoch of osculation | 30 Jun 2025, 13:44 |