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 23080.78531056 .00006299 00000-0 44468-3 0 9990
2 00022 50.2816 46.8877 0128776 154.5791 206.1567 14.99665661621202
| Epoch (UTC): | 21 March 2023 18:50:50 |
| Eccentricity: | 0.0128776 |
| inclination: | 50.2816° |
| perigee height: | 478 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 46.8877° |
| argument of perigee: | 154.5791° |
| revolutions per day: | 14.99665661 |
| mean anomaly at epoch: | 206.1567° |
| orbit number at epoch: | 62120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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