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 24262.72562683 .00000447 00000-0 18725-3 0 9995
2 22826 98.7737 316.3040 0009635 144.9405 215.2414 14.30975864616526
| Epoch (UTC): | 18 September 2024 17:24:54 |
| Eccentricity: | 0.0009635 |
| inclination: | 98.7737° |
| perigee height: | 781 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 316.3040° |
| argument of perigee: | 144.9405° |
| revolutions per day: | 14.30975864 |
| mean anomaly at epoch: | 215.2414° |
| orbit number at epoch: | 61652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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