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 23344.86486616 .00004069 00000-0 27098-3 0 9996
2 00022 50.2790 235.5273 0120851 94.1666 267.3107 15.03525034660887
| Epoch (UTC): | 10 December 2023 20:45:24 |
| Eccentricity: | 0.0120851 |
| inclination: | 50.2790° |
| perigee height: | 472 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 235.5273° |
| argument of perigee: | 94.1666° |
| revolutions per day: | 15.03525034 |
| mean anomaly at epoch: | 267.3107° |
| orbit number at epoch: | 66088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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