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 58U 60013A 25343.82339220 .00000112 00000-0 43703-4 0 9994
2 58 28.3288 20.5899 0164955 79.7613 282.1489 13.46421470208525
| Epoch (UTC): | 09 December 2025 19:45:41 |
| Eccentricity: | 0.0164955 |
| inclination: | 28.3288° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 20.5899° |
| argument of perigee: | 79.7613° |
| revolutions per day: | 13.46421470 |
| mean anomaly at epoch: | 282.1489° |
| orbit number at epoch: | 20852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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