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 01529U 65051D 24357.84422677 .00000486 00000-0 23141-3 0 9997
2 01529 99.0565 212.2972 0035980 341.5072 18.4795 14.23890592 78399
Epoch (UTC): | 22 December 2024 20:15:41 |
Eccentricity: | 0.0035980 |
inclination: | 99.0565° |
perigee height: | 786 km |
apogee height: | 838 km |
right ascension of ascending node: | 212.2972° |
argument of perigee: | 341.5072° |
revolutions per day: | 14.23890592 |
mean anomaly at epoch: | 18.4795° |
orbit number at epoch: | 7839 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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