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 20560U 90031A 24358.23201722 .00002844 00000-0 39649-3 0 9999
2 20560 89.8512 270.9620 0064442 37.5407 323.0287 14.76069704 32857
Epoch (UTC): | 23 December 2024 05:34:06 |
Eccentricity: | 0.0064442 |
inclination: | 89.8512° |
perigee height: | 596 km |
apogee height: | 687 km |
right ascension of ascending node: | 270.9620° |
argument of perigee: | 37.5407° |
revolutions per day: | 14.76069704 |
mean anomaly at epoch: | 323.0287° |
orbit number at epoch: | 3285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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