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 22227.55423068 .00000639 00000-0 65950-4 0 9999
2 22236 82.5053 77.8010 0015497 217.8554 142.1575 14.88571506586628
| Epoch (UTC): | 15 August 2022 13:18:05 |
| Eccentricity: | 0.0015497 |
| inclination: | 82.5053° |
| perigee height: | 591 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 77.8010° |
| argument of perigee: | 217.8554° |
| revolutions per day: | 14.88571506 |
| mean anomaly at epoch: | 142.1575° |
| orbit number at epoch: | 58662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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