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 29938U 99025JL 24357.52839556 .00000484 00000-0 31315-3 0 9992
2 29938 98.7795 351.1808 0032891 228.4049 247.0384 14.07168455920602
| Epoch (UTC): | 22 December 2024 12:40:53 |
| Eccentricity: | 0.0032891 |
| inclination: | 98.7795° |
| perigee height: | 845 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 351.1808° |
| argument of perigee: | 228.4049° |
| revolutions per day: | 14.07168455 |
| mean anomaly at epoch: | 247.0384° |
| orbit number at epoch: | 92060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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