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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 | 97.883° |
Eccentricity | 0.00055 |
RA ascending node | 15.952 hr |
Argument perigee | 216.717° |
Mean anomaly | 143.368° |
Orbital period | 96.478 min |
Epoch of osculation | 12 May 2025, 13:40 |