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 23079.66998415 .00000227 00000-0 10440-3 0 9991
2 22826 98.8483 120.9498 0008152 317.5122 42.5428 14.30623917537907
Epoch (UTC): | 20 March 2023 16:04:46 |
Eccentricity: | 0.0008152 |
inclination: | 98.8483° |
perigee height: | 784 km |
apogee height: | 795 km |
right ascension of ascending node: | 120.9498° |
argument of perigee: | 317.5122° |
revolutions per day: | 14.30623917 |
mean anomaly at epoch: | 42.5428° |
orbit number at epoch: | 53790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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