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 22566U 93016B 22228.82199649 -.00000073 00000-0 -13132-4 0 9990
2 22566 71.0066 66.6602 0009261 154.0963 206.0625 14.15004669518130
| Epoch (UTC): | 16 August 2022 19:43:40 |
| Eccentricity: | 0.0009261 |
| inclination: | 71.0066° |
| perigee height: | 835 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 66.6602° |
| argument of perigee: | 154.0963° |
| revolutions per day: | 14.15004669 |
| mean anomaly at epoch: | 206.0625° |
| orbit number at epoch: | 51813 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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