View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00051U 60009C 25134.16872347 -.00000039 00000-0 45234-3 0 9998
2 00051 47.2107 204.0513 0106532 91.1616 270.1379 12.18358475882523
Epoch (UTC): | 14 May 2025 04:02:57 |
Eccentricity: | 0.0106532 |
inclination: | 47.2107° |
perigee height: | 1515 km |
apogee height: | 1684 km |
right ascension of ascending node: | 204.0513° |
argument of perigee: | 91.1616° |
revolutions per day: | 12.18358475 |
mean anomaly at epoch: | 270.1379° |
orbit number at epoch: | 88252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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