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 24358.10262313 .00004752 00000-0 44716-3 0 9997
2 22236 82.5054 341.1846 0013340 229.3510 130.6551 14.93621643735860
| Epoch (UTC): | 23 December 2024 02:27:46 |
| Eccentricity: | 0.0013340 |
| inclination: | 82.5054° |
| perigee height: | 577 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 341.1846° |
| argument of perigee: | 229.3510° |
| revolutions per day: | 14.93621643 |
| mean anomaly at epoch: | 130.6551° |
| orbit number at epoch: | 73586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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