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 32191U 99025CUM 24257.40412911 .00016291 00000-0 72176-2 0 9997
2 32191 98.7436 311.3374 0100460 66.3952 294.7735 14.20479505883709
Epoch (UTC): | 13 September 2024 09:41:56 |
Eccentricity: | 0.0100460 |
inclination: | 98.7436° |
perigee height: | 751 km |
apogee height: | 896 km |
right ascension of ascending node: | 311.3374° |
argument of perigee: | 66.3952° |
revolutions per day: | 14.20479505 |
mean anomaly at epoch: | 294.7735° |
orbit number at epoch: | 88370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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