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 22376U 92093BR 22222.68747253 .00001078 00000-0 50432-3 0 9998
2 22376 70.8909 172.7066 0060645 27.6060 36.5894 14.21616384525841
| Epoch (UTC): | 10 August 2022 16:29:57 |
| Eccentricity: | 0.0060645 |
| inclination: | 70.8909° |
| perigee height: | 776 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 172.7066° |
| argument of perigee: | 27.6060° |
| revolutions per day: | 14.21616384 |
| mean anomaly at epoch: | 36.5894° |
| orbit number at epoch: | 52584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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