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 24292U 96050B 23271.04081346 .00000013 00000-0 -68822-3 0 9994
2 24292 62.8012 163.5315 5545925 251.4826 42.9359 4.14710829410033
| Epoch (UTC): | 28 September 2023 00:58:46 |
| Eccentricity: | 0.5545925 |
| inclination: | 62.8012° |
| perigee height: | 911 km |
| apogee height: | 19062 km |
| right ascension of ascending node: | 163.5315° |
| argument of perigee: | 251.4826° |
| revolutions per day: | 4.14710829 |
| mean anomaly at epoch: | 42.9359° |
| orbit number at epoch: | 41003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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