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 22178.49057055 .00001535 00000-0 16511-3 0 9996
2 40032 97.9383 111.3115 0012464 28.7289 331.4612 14.89963119435111
| Epoch (UTC): | 27 June 2022 11:46:25 |
| Eccentricity: | 0.0012464 |
| inclination: | 97.9383° |
| perigee height: | 589 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 111.3115° |
| argument of perigee: | 28.7289° |
| revolutions per day: | 14.89963119 |
| mean anomaly at epoch: | 331.4612° |
| orbit number at epoch: | 43511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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