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 24285.86964510 .00000975 00000-0 38755-3 0 9991
2 22826 98.7695 339.6584 0010031 83.9796 276.2529 14.31008809619835
| Epoch (UTC): | 11 October 2024 20:52:17 |
| Eccentricity: | 0.0010031 |
| inclination: | 98.7695° |
| perigee height: | 781 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 339.6584° |
| argument of perigee: | 83.9796° |
| revolutions per day: | 14.31008809 |
| mean anomaly at epoch: | 276.2529° |
| orbit number at epoch: | 61983 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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