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 24259.85881514 .00000695 00000-0 28128-3 0 9995
2 22826 98.7742 313.4104 0009483 152.8110 207.3571 14.30973463615868
| Epoch (UTC): | 15 September 2024 20:36:41 |
| Eccentricity: | 0.0009483 |
| inclination: | 98.7742° |
| perigee height: | 781 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 313.4104° |
| argument of perigee: | 152.8110° |
| revolutions per day: | 14.30973463 |
| mean anomaly at epoch: | 207.3571° |
| orbit number at epoch: | 61586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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