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 38824U 99025EVQ 24354.56043103 .00006813 00000-0 37839-2 0 9990
2 38824 99.2899 109.2929 0102417 123.1512 237.9533 14.08811850682166
| Epoch (UTC): | 19 December 2024 13:27:01 |
| Eccentricity: | 0.0102417 |
| inclination: | 99.2899° |
| perigee height: | 789 km |
| apogee height: | 937 km |
| right ascension of ascending node: | 109.2929° |
| argument of perigee: | 123.1512° |
| revolutions per day: | 14.08811850 |
| mean anomaly at epoch: | 237.9533° |
| orbit number at epoch: | 68216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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