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 25942U 99057C 24357.71111228 .00000817 00000-0 27240-3 0 9990
2 25942 98.7966 28.2390 0097003 22.0363 338.4951 14.37742362317764
| Epoch (UTC): | 22 December 2024 17:04:00 |
| Eccentricity: | 0.0097003 |
| inclination: | 98.7966° |
| perigee height: | 696 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 28.2390° |
| argument of perigee: | 22.0363° |
| revolutions per day: | 14.37742362 |
| mean anomaly at epoch: | 338.4951° |
| orbit number at epoch: | 31776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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