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 32459U 99025DBX 23335.03301888 .00004642 00000-0 11831-2 0 9997
2 32459 98.3560 358.4400 0230562 262.5626 94.9311 14.36337245838641
Epoch (UTC): | 01 December 2023 00:47:32 |
Eccentricity: | 0.0230562 |
inclination: | 98.3560° |
perigee height: | 606 km |
apogee height: | 935 km |
right ascension of ascending node: | 358.4400° |
argument of perigee: | 262.5626° |
revolutions per day: | 14.36337245 |
mean anomaly at epoch: | 94.9311° |
orbit number at epoch: | 83864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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