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 22207U 92073A 24336.86497133 .00000134 00000-0 12810-3 0 9996
2 22207 82.9218 191.9850 0033546 122.4509 248.3800 13.73024286608041
| Epoch (UTC): | 01 December 2024 20:45:33 |
| Eccentricity: | 0.0033546 |
| inclination: | 82.9218° |
| perigee height: | 964 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 191.9850° |
| argument of perigee: | 122.4509° |
| revolutions per day: | 13.73024286 |
| mean anomaly at epoch: | 248.3800° |
| orbit number at epoch: | 60804 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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