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 23083.93626865 .00000329 00000-0 14367-3 0 9998
2 22826 98.8474 125.2902 0008000 303.7745 56.2675 14.30627194538510
Epoch (UTC): | 24 March 2023 22:28:13 |
Eccentricity: | 0.0008000 |
inclination: | 98.8474° |
perigee height: | 784 km |
apogee height: | 795 km |
right ascension of ascending node: | 125.2902° |
argument of perigee: | 303.7745° |
revolutions per day: | 14.30627194 |
mean anomaly at epoch: | 56.2675° |
orbit number at epoch: | 53851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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