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 25189.35990506 .00001360 00000-0 12210-3 0 9995
2 22236 82.5051 152.8286 0013043 296.7985 63.1902 14.94945786744279
| Epoch (UTC): | 08 July 2025 08:38:15 |
| Eccentricity: | 0.0013043 |
| inclination: | 82.5051° |
| perigee height: | 573 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 152.8286° |
| argument of perigee: | 296.7985° |
| revolutions per day: | 14.94945786 |
| mean anomaly at epoch: | 63.1902° |
| orbit number at epoch: | 74427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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