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 24286.50733416 .00002791 00000-0 37048-3 0 9997
2 25861 98.0757 333.2942 0016390 117.8424 242.4450 14.80543258360899
| Epoch (UTC): | 12 October 2024 12:10:33 |
| Eccentricity: | 0.0016390 |
| inclination: | 98.0757° |
| perigee height: | 616 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 333.2942° |
| argument of perigee: | 117.8424° |
| revolutions per day: | 14.80543258 |
| mean anomaly at epoch: | 242.4450° |
| orbit number at epoch: | 36089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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