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 23333.71649897 .00000331 00000-0 14504-3 0 9997
2 22825 98.8199 19.1031 0007548 309.3164 50.7348 14.30387788574226
| Epoch (UTC): | 29 November 2023 17:11:45 |
| Eccentricity: | 0.0007548 |
| inclination: | 98.8199° |
| perigee height: | 785 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 19.1031° |
| argument of perigee: | 309.3164° |
| revolutions per day: | 14.30387788 |
| mean anomaly at epoch: | 50.7348° |
| orbit number at epoch: | 57422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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