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 25187.95429535 .00001395 00000-0 12533-3 0 9994
2 22236 82.5050 154.1717 0013134 302.0979 57.8967 14.94941543744062
| Epoch (UTC): | 06 July 2025 22:54:11 |
| Eccentricity: | 0.0013134 |
| inclination: | 82.5050° |
| perigee height: | 573 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 154.1717° |
| argument of perigee: | 302.0979° |
| revolutions per day: | 14.94941543 |
| mean anomaly at epoch: | 57.8967° |
| orbit number at epoch: | 74406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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