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 22177.81900124 .00001640 00000-0 17600-3 0 9992
2 40032 97.9383 110.6372 0012522 30.7880 329.4069 14.89961507435014
| Epoch (UTC): | 26 June 2022 19:39:21 |
| Eccentricity: | 0.0012522 |
| inclination: | 97.9383° |
| perigee height: | 589 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 110.6372° |
| argument of perigee: | 30.7880° |
| revolutions per day: | 14.89961507 |
| mean anomaly at epoch: | 329.4069° |
| orbit number at epoch: | 43501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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