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 14780U 84021A 22142.25933358 .00002092 00000-0 19285-3 0 9995
2 14780 98.2053 339.0182 0088865 14.3966 345.9753 14.92949716568747
Epoch (UTC): | 22 May 2022 06:13:26 |
Eccentricity: | 0.0088865 |
inclination: | 98.2053° |
perigee height: | 527 km |
apogee height: | 650 km |
right ascension of ascending node: | 339.0182° |
argument of perigee: | 14.3966° |
revolutions per day: | 14.92949716 |
mean anomaly at epoch: | 345.9753° |
orbit number at epoch: | 56874 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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