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 19046U 88032B 22144.89873524 .00002198 00000-0 16267-3 0 9995
2 19046 97.3903 144.8926 0035645 321.5056 38.3629 15.03663423843078
| Epoch (UTC): | 24 May 2022 21:34:10 |
| Eccentricity: | 0.0035645 |
| inclination: | 97.3903° |
| perigee height: | 531 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 144.8926° |
| argument of perigee: | 321.5056° |
| revolutions per day: | 15.03663423 |
| mean anomaly at epoch: | 38.3629° |
| orbit number at epoch: | 84307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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