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 25346.96957131 .00002790 00000-0 32357-3 0 9991
2 00107 28.7835 309.3653 0498512 190.2614 168.7446 14.21016906249971
| Epoch (UTC): | 12 December 2025 23:16:10 |
| Eccentricity: | 0.0498512 |
| inclination: | 28.7835° |
| perigee height: | 463 km |
| apogee height: | 1181 km |
| right ascension of ascending node: | 309.3653° |
| argument of perigee: | 190.2614° |
| revolutions per day: | 14.21016906 |
| mean anomaly at epoch: | 168.7446° |
| orbit number at epoch: | 24997 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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