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 22826U 93061D 23334.72669011 .00000419 00000-0 17743-3 0 9995
2 22826 98.8144 19.9888 0007947 289.6477 70.3847 14.30758998574626
| Epoch (UTC): | 30 November 2023 17:26:26 |
| Eccentricity: | 0.0007947 |
| inclination: | 98.8144° |
| perigee height: | 783 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 19.9888° |
| argument of perigee: | 289.6477° |
| revolutions per day: | 14.30758998 |
| mean anomaly at epoch: | 70.3847° |
| orbit number at epoch: | 57462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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