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 23339.28186298 .00008009 00000-0 51384-3 0 9992
2 00022 50.2792 262.0652 0121001 72.5070 288.9063 15.03458106660045
| Epoch (UTC): | 05 December 2023 06:45:52 |
| Eccentricity: | 0.0121001 |
| inclination: | 50.2792° |
| perigee height: | 472 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 262.0652° |
| argument of perigee: | 72.5070° |
| revolutions per day: | 15.03458106 |
| mean anomaly at epoch: | 288.9063° |
| orbit number at epoch: | 66004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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