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 00107U 61013A 23038.57476028 .00005188 00000-0 66974-3 0 9991
2 00107 28.7910 125.2347 0537377 296.1181 58.5063 14.11307804102527
| Epoch (UTC): | 07 February 2023 13:47:39 |
| Eccentricity: | 0.0537377 |
| inclination: | 28.7910° |
| perigee height: | 466 km |
| apogee height: | 1243 km |
| right ascension of ascending node: | 125.2347° |
| argument of perigee: | 296.1181° |
| revolutions per day: | 14.11307804 |
| mean anomaly at epoch: | 58.5063° |
| orbit number at epoch: | 10252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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