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 35123U 99025DLB 24352.71545928 .00002204 00000-0 99226-3 0 9995
2 35123 99.1046 156.3381 0050993 26.9683 333.4127 14.22666862559513
| Epoch (UTC): | 17 December 2024 17:10:15 |
| Eccentricity: | 0.0050993 |
| inclination: | 99.1046° |
| perigee height: | 779 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 156.3381° |
| argument of perigee: | 26.9683° |
| revolutions per day: | 14.22666862 |
| mean anomaly at epoch: | 333.4127° |
| orbit number at epoch: | 55951 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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