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 22590U 93020A 23082.83166449 .00000085 00000-0 72697-4 0 9996
2 22590 82.9285 298.0916 0022903 354.5202 18.1779 13.75465581504373
| Epoch (UTC): | 23 March 2023 19:57:35 |
| Eccentricity: | 0.0022903 |
| inclination: | 82.9285° |
| perigee height: | 963 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 298.0916° |
| argument of perigee: | 354.5202° |
| revolutions per day: | 13.75465581 |
| mean anomaly at epoch: | 18.1779° |
| orbit number at epoch: | 50437 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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