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 23334.84834283 .00000121 00000-0 58694-4 0 9998
2 00058 28.3249 175.1184 0164796 72.6836 289.1666 13.46362779108729
| Epoch (UTC): | 30 November 2023 20:21:36 |
| Eccentricity: | 0.0164796 |
| inclination: | 28.3249° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 175.1184° |
| argument of perigee: | 72.6836° |
| revolutions per day: | 13.46362779 |
| mean anomaly at epoch: | 289.1666° |
| orbit number at epoch: | 10872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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