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 00058U 60013A 25340.48682227 .00000104 00000-0 33486-4 0 9999
2 00058 28.3286 37.5195 0164938 52.1292 309.4050 13.46421250208072
| Epoch (UTC): | 06 December 2025 11:41:01 |
| Eccentricity: | 0.0164938 |
| inclination: | 28.3286° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 37.5195° |
| argument of perigee: | 52.1292° |
| revolutions per day: | 13.46421250 |
| mean anomaly at epoch: | 309.4050° |
| orbit number at epoch: | 20807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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