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 15055U 84062A 23273.76420873 .00000044 00000-0 31281-4 0 9997
2 15055 82.9530 89.7486 0026156 293.8991 77.6126 13.74403570969702
Epoch (UTC): | 30 September 2023 18:20:27 |
Eccentricity: | 0.0026156 |
inclination: | 82.9530° |
perigee height: | 964 km |
apogee height: | 1003 km |
right ascension of ascending node: | 89.7486° |
argument of perigee: | 293.8991° |
revolutions per day: | 13.74403570 |
mean anomaly at epoch: | 77.6126° |
orbit number at epoch: | 96970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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