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 24287.21032528 .00000162 00000-0 10786-3 0 9990
2 22566 71.0072 211.4488 0009649 11.0223 349.1109 14.15174960629669
| Epoch (UTC): | 13 October 2024 05:02:52 |
| Eccentricity: | 0.0009649 |
| inclination: | 71.0072° |
| perigee height: | 835 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 211.4488° |
| argument of perigee: | 11.0223° |
| revolutions per day: | 14.15174960 |
| mean anomaly at epoch: | 349.1109° |
| orbit number at epoch: | 62966 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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