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 24817U 94029ABU 24276.84057531 .00019281 00000-0 50994-2 0 9990
2 24817 81.6921 221.9855 0389088 92.8114 301.4296 14.12067579432549
| Epoch (UTC): | 02 October 2024 20:10:25 |
| Eccentricity: | 0.0389088 |
| inclination: | 81.6921° |
| perigee height: | 571 km |
| apogee height: | 1133 km |
| right ascension of ascending node: | 221.9855° |
| argument of perigee: | 92.8114° |
| revolutions per day: | 14.12067579 |
| mean anomaly at epoch: | 301.4296° |
| orbit number at epoch: | 43254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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