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 25340.71883469 .00002922 00000-0 34187-3 0 9990
2 00107 28.7829 345.3425 0498800 131.9898 232.4271 14.20988339249081
| Epoch (UTC): | 06 December 2025 17:15:07 |
| Eccentricity: | 0.0498800 |
| inclination: | 28.7829° |
| perigee height: | 463 km |
| apogee height: | 1181 km |
| right ascension of ascending node: | 345.3425° |
| argument of perigee: | 131.9898° |
| revolutions per day: | 14.20988339 |
| mean anomaly at epoch: | 232.4271° |
| orbit number at epoch: | 24908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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