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 22180.57242950 .00001187 00000-0 12904-3 0 9993
2 40032 97.9383 113.4019 0012277 22.3182 337.8568 14.89967924435423
| Epoch (UTC): | 29 June 2022 13:44:17 |
| Eccentricity: | 0.0012277 |
| inclination: | 97.9383° |
| perigee height: | 589 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 113.4019° |
| argument of perigee: | 22.3182° |
| revolutions per day: | 14.89967924 |
| mean anomaly at epoch: | 337.8568° |
| orbit number at epoch: | 43542 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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