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 25197.85546346 -.00000252 00000-0 -10476-3 0 9997
2 22566 71.0089 350.4862 0011953 313.7132 46.2999 14.15263418668807
| Epoch (UTC): | 16 July 2025 20:31:52 |
| Eccentricity: | 0.0011953 |
| inclination: | 71.0089° |
| perigee height: | 833 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 350.4862° |
| argument of perigee: | 313.7132° |
| revolutions per day: | 14.15263418 |
| mean anomaly at epoch: | 46.2999° |
| orbit number at epoch: | 66880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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