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 22236U 92080A 25191.36791345 .00001200 00000-0 10748-3 0 9996
2 22236 82.5053 150.9100 0012962 289.3177 70.6642 14.94950645744572
| Epoch (UTC): | 10 July 2025 08:49:47 |
| Eccentricity: | 0.0012962 |
| inclination: | 82.5053° |
| perigee height: | 573 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 150.9100° |
| argument of perigee: | 289.3177° |
| revolutions per day: | 14.94950645 |
| mean anomaly at epoch: | 70.6642° |
| orbit number at epoch: | 74457 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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