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 24260.69788281 .00000551 00000-0 22673-3 0 9996
2 22826 98.7741 314.2574 0009538 150.4767 209.6955 14.30973801615980
| Epoch (UTC): | 16 September 2024 16:44:57 |
| Eccentricity: | 0.0009538 |
| inclination: | 98.7741° |
| perigee height: | 781 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 314.2574° |
| argument of perigee: | 150.4767° |
| revolutions per day: | 14.30973801 |
| mean anomaly at epoch: | 209.6955° |
| orbit number at epoch: | 61598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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