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 23333.55252176 .00003347 00000-0 33872-3 0 9994
2 22236 82.5063 351.6455 0017545 95.2043 265.1179 14.90589889656734
| Epoch (UTC): | 29 November 2023 13:15:37 |
| Eccentricity: | 0.0017545 |
| inclination: | 82.5063° |
| perigee height: | 584 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 351.6455° |
| argument of perigee: | 95.2043° |
| revolutions per day: | 14.90589889 |
| mean anomaly at epoch: | 265.1179° |
| orbit number at epoch: | 65673 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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