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 22286U 92094A 23156.38646984 .00001957 00000-0 19918-3 0 9992
2 22286 82.5187 117.1519 0022407 81.6058 278.7700 14.90078011625556
| Epoch (UTC): | 05 June 2023 09:16:30 |
| Eccentricity: | 0.0022407 |
| inclination: | 82.5187° |
| perigee height: | 582 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 117.1519° |
| argument of perigee: | 81.6058° |
| revolutions per day: | 14.90078011 |
| mean anomaly at epoch: | 278.7700° |
| orbit number at epoch: | 62555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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