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 21107.55760205 .00000211 00000-0 20013-4 0 9999
2 22286 82.5177 132.8990 0021971 147.3442 212.9140 14.88259199509671
| Epoch (UTC): | 17 April 2021 13:22:56 |
| Eccentricity: | 0.0021971 |
| inclination: | 82.5177° |
| perigee height: | 588 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 132.8990° |
| argument of perigee: | 147.3442° |
| revolutions per day: | 14.88259199 |
| mean anomaly at epoch: | 212.9140° |
| orbit number at epoch: | 50967 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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