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 25346.17678030 .00001010 00000-0 13526-3 0 9996
2 25861 98.0127 40.3279 0014876 176.4520 183.6801 14.81585442423904
| Epoch (UTC): | 12 December 2025 04:14:33 |
| Eccentricity: | 0.0014876 |
| inclination: | 98.0127° |
| perigee height: | 614 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 40.3279° |
| argument of perigee: | 176.4520° |
| revolutions per day: | 14.81585442 |
| mean anomaly at epoch: | 183.6801° |
| orbit number at epoch: | 42390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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