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 29993U 99025LT 24277.88969146 .00000882 00000-0 54061-3 0 9997
2 29993 98.8535 318.4370 0040453 97.9988 262.5775 14.07918498910504
| Epoch (UTC): | 03 October 2024 21:21:09 |
| Eccentricity: | 0.0040453 |
| inclination: | 98.8535° |
| perigee height: | 837 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 318.4370° |
| argument of perigee: | 97.9988° |
| revolutions per day: | 14.07918498 |
| mean anomaly at epoch: | 262.5775° |
| orbit number at epoch: | 91050 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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