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 107U 61013A 25339.17358385 .00003333 00000-0 39306-3 0 9997
2 107 28.7830 354.2355 0498853 117.5921 247.6214 14.20981115248864
| Epoch (UTC): | 05 December 2025 04:09:57 |
| Eccentricity: | 0.0498853 |
| inclination: | 28.7830° |
| perigee height: | 463 km |
| apogee height: | 1181 km |
| right ascension of ascending node: | 354.2355° |
| argument of perigee: | 117.5921° |
| revolutions per day: | 14.20981115 |
| mean anomaly at epoch: | 247.6214° |
| orbit number at epoch: | 24886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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