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 25340.36764765 .00003040 00000-0 35658-3 0 9994
2 00107 28.7829 347.3636 0498814 128.7172 235.9086 14.20986721249031
| Epoch (UTC): | 06 December 2025 08:49:24 |
| Eccentricity: | 0.0498814 |
| inclination: | 28.7829° |
| perigee height: | 463 km |
| apogee height: | 1181 km |
| right ascension of ascending node: | 347.3636° |
| argument of perigee: | 128.7172° |
| revolutions per day: | 14.20986721 |
| mean anomaly at epoch: | 235.9086° |
| orbit number at epoch: | 24903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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