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 31966U 99025CNT 22224.81961133 .00001326 00000-0 33919-3 0 9994
2 31966 99.0385 266.5120 0118028 4.4972 355.7251 14.48268727480200
| Epoch (UTC): | 12 August 2022 19:40:14 |
| Eccentricity: | 0.0118028 |
| inclination: | 99.0385° |
| perigee height: | 647 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 266.5120° |
| argument of perigee: | 4.4972° |
| revolutions per day: | 14.48268727 |
| mean anomaly at epoch: | 355.7251° |
| orbit number at epoch: | 48020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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