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 15890U 85058B 22145.11057946 .00000458 00000-0 52444-4 0 9996
2 15890 82.5281 13.2735 0021824 39.0482 321.2303 14.83600704992192
Epoch (UTC): | 25 May 2022 02:39:14 |
Eccentricity: | 0.0021824 |
inclination: | 82.5281° |
perigee height: | 603 km |
apogee height: | 633 km |
right ascension of ascending node: | 13.2735° |
argument of perigee: | 39.0482° |
revolutions per day: | 14.83600704 |
mean anomaly at epoch: | 321.2303° |
orbit number at epoch: | 99219 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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