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 12544U 81057A 25012.37403389 .00000002 00000-0 00000-0 0 9996
2 12544 11.1541 322.7370 0029422 2.3616 187.5549 0.98722584118703
Epoch (UTC): | 12 January 2025 08:58:36 |
Eccentricity: | 0.0029422 |
inclination: | 11.1541° |
perigee height: | 36101 km |
apogee height: | 36351 km |
right ascension of ascending node: | 322.7370° |
argument of perigee: | 2.3616° |
revolutions per day: | 0.98722584 |
mean anomaly at epoch: | 187.5549° |
orbit number at epoch: | 11870 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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