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 25344.41655134 .00000113 00000-0 46050-4 0 9994
2 58 28.3287 17.5803 0164957 84.6746 277.2596 13.46421507208603
| Epoch (UTC): | 10 December 2025 09:59:50 |
| Eccentricity: | 0.0164957 |
| inclination: | 28.3287° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 17.5803° |
| argument of perigee: | 84.6746° |
| revolutions per day: | 13.46421507 |
| mean anomaly at epoch: | 277.2596° |
| orbit number at epoch: | 20860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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