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 59112U 24043Q 25312.62421833 .00039593 00000-0 90826-3 0 9990
2 59112 97.5322 87.6721 0008850 289.6056 70.4235 15.42587266 93713
| Epoch (UTC): | 08 November 2025 14:58:52 |
| Eccentricity: | 0.0008850 |
| inclination: | 97.5322° |
| perigee height: | 432 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 87.6721° |
| argument of perigee: | 289.6056° |
| revolutions per day: | 15.42587266 |
| mean anomaly at epoch: | 70.4235° |
| orbit number at epoch: | 9371 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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