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 40024U 14033Q 22182.83361868 .00001022 00000-0 10713-3 0 9999
2 40024 97.9862 126.5905 0012197 8.0064 352.1347 14.91779010436129
| Epoch (UTC): | 01 July 2022 20:00:24 |
| Eccentricity: | 0.0012197 |
| inclination: | 97.9862° |
| perigee height: | 584 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 126.5905° |
| argument of perigee: | 8.0064° |
| revolutions per day: | 14.91779010 |
| mean anomaly at epoch: | 352.1347° |
| orbit number at epoch: | 43612 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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