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 14781U 84021B 23085.90603869 .00002921 00000-0 35191-3 0 9991
2 14781 97.6512 66.0765 0009885 108.7202 251.5087 14.84556236 81936
Epoch (UTC): | 26 March 2023 21:44:41 |
Eccentricity: | 0.0009885 |
inclination: | 97.6512° |
perigee height: | 608 km |
apogee height: | 622 km |
right ascension of ascending node: | 66.0765° |
argument of perigee: | 108.7202° |
revolutions per day: | 14.84556236 |
mean anomaly at epoch: | 251.5087° |
orbit number at epoch: | 8193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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