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 33591U 09005A 23086.16822330 .00000326 00000-0 20042-3 0 9991
2 33591 99.1109 130.7468 0014830 112.9343 247.3395 14.12718653728367
Epoch (UTC): | 27 March 2023 04:02:14 |
Eccentricity: | 0.0014830 |
inclination: | 99.1109° |
perigee height: | 839 km |
apogee height: | 861 km |
right ascension of ascending node: | 130.7468° |
argument of perigee: | 112.9343° |
revolutions per day: | 14.12718653 |
mean anomaly at epoch: | 247.3395° |
orbit number at epoch: | 72836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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