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 19826U 89017A 23088.46579464 .00000139 00000-0 13627-3 0 9992
2 19826 82.9498 69.3689 0028751 277.1569 199.8119 13.72368610707211
Epoch (UTC): | 29 March 2023 11:10:44 |
Eccentricity: | 0.0028751 |
inclination: | 82.9498° |
perigee height: | 970 km |
apogee height: | 1012 km |
right ascension of ascending node: | 69.3689° |
argument of perigee: | 277.1569° |
revolutions per day: | 13.72368610 |
mean anomaly at epoch: | 199.8119° |
orbit number at epoch: | 70721 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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