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 22237U 92080B 22224.83732702 .00000204 00000-0 24663-4 0 9990
2 22237 82.5140 166.2046 0019965 164.1251 196.0592 14.78578144601517
| Epoch (UTC): | 12 August 2022 20:05:45 |
| Eccentricity: | 0.0019965 |
| inclination: | 82.5140° |
| perigee height: | 620 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 166.2046° |
| argument of perigee: | 164.1251° |
| revolutions per day: | 14.78578144 |
| mean anomaly at epoch: | 196.0592° |
| orbit number at epoch: | 60151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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