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 25193.89742516 -.00000175 00000-0 -65180-4 0 9991
2 22566 71.0090 358.7988 0011787 319.0532 40.9704 14.15264679668240
| Epoch (UTC): | 12 July 2025 21:32:17 |
| Eccentricity: | 0.0011787 |
| inclination: | 71.0090° |
| perigee height: | 833 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 358.7988° |
| argument of perigee: | 319.0532° |
| revolutions per day: | 14.15264679 |
| mean anomaly at epoch: | 40.9704° |
| orbit number at epoch: | 66824 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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