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 24251.74779458 .00000763 00000-0 30728-3 0 9993
2 22826 98.7754 305.2226 0009055 175.7538 184.3722 14.30961810614705
| Epoch (UTC): | 07 September 2024 17:56:49 |
| Eccentricity: | 0.0009055 |
| inclination: | 98.7754° |
| perigee height: | 782 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 305.2226° |
| argument of perigee: | 175.7538° |
| revolutions per day: | 14.30961810 |
| mean anomaly at epoch: | 184.3722° |
| orbit number at epoch: | 61470 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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