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 43678U 18084H 23087.24325464 .00003521 00000-0 34334-3 0 9990
2 43678 98.0071 229.6608 0010779 71.0616 289.1691 14.93092205240189
Epoch (UTC): | 28 March 2023 05:50:17 |
Eccentricity: | 0.0010779 |
inclination: | 98.0071° |
perigee height: | 581 km |
apogee height: | 596 km |
right ascension of ascending node: | 229.6608° |
argument of perigee: | 71.0616° |
revolutions per day: | 14.93092205 |
mean anomaly at epoch: | 289.1691° |
orbit number at epoch: | 24018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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