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 29092U 06015A 24357.85659549 .00001835 00000-0 21460-3 0 9999
2 29092 97.7899 19.5326 0001453 91.4507 268.6875 14.86271298 9355
| Epoch (UTC): | 22 December 2024 20:33:29 |
| Eccentricity: | 0.0001453 |
| inclination: | 97.7899° |
| perigee height: | 608 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 19.5326° |
| argument of perigee: | 91.4507° |
| revolutions per day: | 14.86271298 |
| mean anomaly at epoch: | 268.6875° |
| orbit number at epoch: | 935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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