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 22825U 93061C 24260.39426605 .00000566 00000-0 23441-3 0 9991
2 22825 98.7795 314.0842 0008732 165.3010 194.8427 14.30583056615657
| Epoch (UTC): | 16 September 2024 09:27:44 |
| Eccentricity: | 0.0008732 |
| inclination: | 98.7795° |
| perigee height: | 783 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 314.0842° |
| argument of perigee: | 165.3010° |
| revolutions per day: | 14.30583056 |
| mean anomaly at epoch: | 194.8427° |
| orbit number at epoch: | 61565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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