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 22221.87726901 .00001895 00000-0 15675-3 0 9996
2 00022 50.2832 22.4933 0134149 15.0877 345.4013 14.97269973587635
| Epoch (UTC): | 09 August 2022 21:03:16 |
| Eccentricity: | 0.0134149 |
| inclination: | 50.2832° |
| perigee height: | 482 km |
| apogee height: | 668 km |
| right ascension of ascending node: | 22.4933° |
| argument of perigee: | 15.0877° |
| revolutions per day: | 14.97269973 |
| mean anomaly at epoch: | 345.4013° |
| orbit number at epoch: | 58763 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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