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 52757U 22057AB 24357.82320184 .00017069 00000-0 57925-3 0 9995
2 52757 97.5955 122.3016 0007759 200.0407 160.0530 15.30558734142995
Epoch (UTC): | 22 December 2024 19:45:24 |
Eccentricity: | 0.0007759 |
inclination: | 97.5955° |
perigee height: | 469 km |
apogee height: | 479 km |
right ascension of ascending node: | 122.3016° |
argument of perigee: | 200.0407° |
revolutions per day: | 15.30558734 |
mean anomaly at epoch: | 160.0530° |
orbit number at epoch: | 14299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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