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 25200.89467455 -.00000261 00000-0 -10931-3 0 9995
2 22566 71.0089 344.1034 0012023 309.7031 50.3031 14.15262275669231
| Epoch (UTC): | 19 July 2025 21:28:19 |
| Eccentricity: | 0.0012023 |
| inclination: | 71.0089° |
| perigee height: | 833 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 344.1034° |
| argument of perigee: | 309.7031° |
| revolutions per day: | 14.15262275 |
| mean anomaly at epoch: | 50.3031° |
| orbit number at epoch: | 66923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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