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 40032U 14033Y 22175.80428830 .00001558 00000-0 16753-3 0 9994
2 40032 97.9383 108.6142 0012680 36.9426 323.2662 14.89953762434716
| Epoch (UTC): | 24 June 2022 19:18:10 |
| Eccentricity: | 0.0012680 |
| inclination: | 97.9383° |
| perigee height: | 589 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 108.6142° |
| argument of perigee: | 36.9426° |
| revolutions per day: | 14.89953762 |
| mean anomaly at epoch: | 323.2662° |
| orbit number at epoch: | 43471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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