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 25544U 98067A 22187.02687112 .00005927 00000-0 11236-3 0 9996
2 25544 51.6427 243.2821 0004495 336.8418 105.9486 15.49842174348108
| Epoch (UTC): | 06 July 2022 00:38:41 |
| Eccentricity: | 0.0004495 |
| inclination: | 51.6427° |
| perigee height: | 414 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 243.2821° |
| argument of perigee: | 336.8418° |
| revolutions per day: | 15.49842174 |
| mean anomaly at epoch: | 105.9486° |
| orbit number at epoch: | 34810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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