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 30654U 99025APL 24357.70668826 .00003834 00000-0 19946-2 0 9996
2 30654 99.2427 261.8031 0037372 19.2051 341.0520 14.14910924916550
| Epoch (UTC): | 22 December 2024 16:57:37 |
| Eccentricity: | 0.0037372 |
| inclination: | 99.2427° |
| perigee height: | 815 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 261.8031° |
| argument of perigee: | 19.2051° |
| revolutions per day: | 14.14910924 |
| mean anomaly at epoch: | 341.0520° |
| orbit number at epoch: | 91655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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