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 25348.23373464 .00002328 00000-0 26613-3 0 9999
2 00107 28.7839 302.0894 0498444 202.0466 155.7949 14.21022397250150
| Epoch (UTC): | 14 December 2025 05:36:34 |
| Eccentricity: | 0.0498444 |
| inclination: | 28.7839° |
| perigee height: | 463 km |
| apogee height: | 1181 km |
| right ascension of ascending node: | 302.0894° |
| argument of perigee: | 202.0466° |
| revolutions per day: | 14.21022397 |
| mean anomaly at epoch: | 155.7949° |
| orbit number at epoch: | 25015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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