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 20234U 89074C 24357.74925907 .00000026 00000-0 85365-4 0 9992
2 20234 82.5853 232.7103 0005725 105.7590 318.9562 12.62608376625309
| Epoch (UTC): | 22 December 2024 17:58:55 |
| Eccentricity: | 0.0005725 |
| inclination: | 82.5853° |
| perigee height: | 1408 km |
| apogee height: | 1416 km |
| right ascension of ascending node: | 232.7103° |
| argument of perigee: | 105.7590° |
| revolutions per day: | 12.62608376 |
| mean anomaly at epoch: | 318.9562° |
| orbit number at epoch: | 62530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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