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 59588U 24077B 25340.18107068 .00053165 00000-0 45635-1 0 9994
2 59588 97.2742 297.2508 0077735 352.6662 7.3356 13.85019149 81239
| Epoch (UTC): | 06 December 2025 04:20:44 |
| Eccentricity: | 0.0077735 |
| inclination: | 97.2742° |
| perigee height: | 889 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 297.2508° |
| argument of perigee: | 352.6662° |
| revolutions per day: | 13.85019149 |
| mean anomaly at epoch: | 7.3356° |
| orbit number at epoch: | 8123 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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