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 25861U 99039B 25343.13763400 .00000997 00000-0 13359-3 0 9992
2 25861 98.0129 37.2885 0014643 186.4383 173.6643 14.81577920423459
| Epoch (UTC): | 09 December 2025 03:18:11 |
| Eccentricity: | 0.0014643 |
| inclination: | 98.0129° |
| perigee height: | 614 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 37.2885° |
| argument of perigee: | 186.4383° |
| revolutions per day: | 14.81577920 |
| mean anomaly at epoch: | 173.6643° |
| orbit number at epoch: | 42345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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