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 22286U 92094A 25193.20733751 .00001486 00000-0 13035-3 0 9996
2 22286 82.5188 107.3089 0019634 35.8081 324.4452 14.95804923761160
| Epoch (UTC): | 12 July 2025 04:58:33 |
| Eccentricity: | 0.0019634 |
| inclination: | 82.5188° |
| perigee height: | 566 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 107.3089° |
| argument of perigee: | 35.8081° |
| revolutions per day: | 14.95804923 |
| mean anomaly at epoch: | 324.4452° |
| orbit number at epoch: | 76116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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