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 23339.51962769 .00000124 00000-0 60828-4 0 9993
2 00058 28.3247 151.4155 0164804 111.3875 250.4338 13.46363259109357
| Epoch (UTC): | 05 December 2023 12:28:15 |
| Eccentricity: | 0.0164804 |
| inclination: | 28.3247° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 151.4155° |
| argument of perigee: | 111.3875° |
| revolutions per day: | 13.46363259 |
| mean anomaly at epoch: | 250.4338° |
| orbit number at epoch: | 10935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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