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 00022U 59009A 22145.85132373 .00006165 00000-0 46264-3 0 9996
2 00022 50.2833 20.2946 0135221 83.7591 277.8741 14.96864649576244
| Epoch (UTC): | 25 May 2022 20:25:54 |
| Eccentricity: | 0.0135221 |
| inclination: | 50.2833° |
| perigee height: | 482 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 20.2946° |
| argument of perigee: | 83.7591° |
| revolutions per day: | 14.96864649 |
| mean anomaly at epoch: | 277.8741° |
| orbit number at epoch: | 57624 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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