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 25196.92336978 .00001291 00000-0 11569-3 0 9992
2 22236 82.5058 145.6020 0012860 268.2318 91.7430 14.94965696745403
| Epoch (UTC): | 15 July 2025 22:09:39 |
| Eccentricity: | 0.0012860 |
| inclination: | 82.5058° |
| perigee height: | 573 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 145.6020° |
| argument of perigee: | 268.2318° |
| revolutions per day: | 14.94965696 |
| mean anomaly at epoch: | 91.7430° |
| orbit number at epoch: | 74540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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