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 24299U 96051C 24357.61291797 .00000079 00000-0 11046-3 0 9991
2 24299 71.0378 60.1130 0187282 70.0487 292.0679 13.75660138420235
| Epoch (UTC): | 22 December 2024 14:42:36 |
| Eccentricity: | 0.0187282 |
| inclination: | 71.0378° |
| perigee height: | 841 km |
| apogee height: | 1117 km |
| right ascension of ascending node: | 60.1130° |
| argument of perigee: | 70.0487° |
| revolutions per day: | 13.75660138 |
| mean anomaly at epoch: | 292.0679° |
| orbit number at epoch: | 42023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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