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 30565U 99025ALF 24357.62545694 .00007083 00000-0 38932-2 0 9991
2 30565 98.4724 243.4495 0148307 288.1645 99.7305 14.06530050909288
| Epoch (UTC): | 22 December 2024 15:00:39 |
| Eccentricity: | 0.0148307 |
| inclination: | 98.4724° |
| perigee height: | 764 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 243.4495° |
| argument of perigee: | 288.1645° |
| revolutions per day: | 14.06530050 |
| mean anomaly at epoch: | 99.7305° |
| orbit number at epoch: | 90928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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