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 23030.53013889 .00004091 00000-0 30144-3 0 9991
2 00022 50.2819 284.2152 0129963 321.4287 37.7430 14.98928893613669
| Epoch (UTC): | 30 January 2023 12:43:24 |
| Eccentricity: | 0.0129963 |
| inclination: | 50.2819° |
| perigee height: | 480 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 284.2152° |
| argument of perigee: | 321.4287° |
| revolutions per day: | 14.98928893 |
| mean anomaly at epoch: | 37.7430° |
| orbit number at epoch: | 61366 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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