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 22219.54128901 .00001136 00000-0 10305-3 0 9996
2 00022 50.2843 33.4899 0134178 6.1391 354.1164 14.97260139587284
| Epoch (UTC): | 07 August 2022 12:59:27 |
| Eccentricity: | 0.0134178 |
| inclination: | 50.2843° |
| perigee height: | 482 km |
| apogee height: | 668 km |
| right ascension of ascending node: | 33.4899° |
| argument of perigee: | 6.1391° |
| revolutions per day: | 14.97260139 |
| mean anomaly at epoch: | 354.1164° |
| orbit number at epoch: | 58728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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