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 22U 59009A 22224.14648930 .00001620 00000-0 13736-3 0 9996
2 22 50.2834 11.8106 0134096 23.7763 336.9304 14.97279245342935
| Epoch (UTC): | 12 August 2022 03:30:56 |
| Eccentricity: | 0.0134096 |
| inclination: | 50.2834° |
| perigee height: | 482 km |
| apogee height: | 668 km |
| right ascension of ascending node: | 11.8106° |
| argument of perigee: | 23.7763° |
| revolutions per day: | 14.97279245 |
| mean anomaly at epoch: | 336.9304° |
| orbit number at epoch: | 34293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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