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 22179.49792270 .00001384 00000-0 14946-3 0 9994
2 40032 97.9383 112.3230 0012375 25.6227 334.5601 14.89965543435260
| Epoch (UTC): | 28 June 2022 11:57:00 |
| Eccentricity: | 0.0012375 |
| inclination: | 97.9383° |
| perigee height: | 589 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 112.3230° |
| argument of perigee: | 25.6227° |
| revolutions per day: | 14.89965543 |
| mean anomaly at epoch: | 334.5601° |
| orbit number at epoch: | 43526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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