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 23336.85034372 .00000134 00000-0 76631-4 0 9997
2 00058 28.3247 164.9604 0164813 89.2562 272.6863 13.46363141108999
| Epoch (UTC): | 02 December 2023 20:24:29 |
| Eccentricity: | 0.0164813 |
| inclination: | 28.3247° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 164.9604° |
| argument of perigee: | 89.2562° |
| revolutions per day: | 13.46363141 |
| mean anomaly at epoch: | 272.6863° |
| orbit number at epoch: | 10899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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