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 10515U 77117B 22227.51994373 .00000185 00000-0 99905-4 0 9991
2 10515 81.2426 247.0726 0030056 321.0263 38.8741 14.08759712295243
Epoch (UTC): | 15 August 2022 12:28:43 |
Eccentricity: | 0.0030056 |
inclination: | 81.2426° |
perigee height: | 842 km |
apogee height: | 885 km |
right ascension of ascending node: | 247.0726° |
argument of perigee: | 321.0263° |
revolutions per day: | 14.08759712 |
mean anomaly at epoch: | 38.8741° |
orbit number at epoch: | 29524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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