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 25137.78151926 .00009689 00000-0 42601-3 0 9992
2 00022 50.2746 239.1759 0092946 342.7591 17.0216 15.18665304740060
| Epoch (UTC): | 17 May 2025 18:45:23 |
| Eccentricity: | 0.0092946 |
| inclination: | 50.2746° |
| perigee height: | 446 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 239.1759° |
| argument of perigee: | 342.7591° |
| revolutions per day: | 15.18665304 |
| mean anomaly at epoch: | 17.0216° |
| orbit number at epoch: | 74006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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