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 19922U 89028B 22228.18935863 .00000082 00000-0 66603-4 0 9994
2 19922 82.9576 107.6431 0036730 4.8517 355.2989 13.77258158676825
| Epoch (UTC): | 16 August 2022 04:32:40 |
| Eccentricity: | 0.0036730 |
| inclination: | 82.9576° |
| perigee height: | 946 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 107.6431° |
| argument of perigee: | 4.8517° |
| revolutions per day: | 13.77258158 |
| mean anomaly at epoch: | 355.2989° |
| orbit number at epoch: | 67682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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