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 35459U 93036ALD 23330.88680421 .00001540 00000-0 54802-3 0 9997
2 35459 73.8694 132.8862 0018007 231.5289 128.4248 14.35117057759364
Epoch (UTC): | 26 November 2023 21:16:59 |
Eccentricity: | 0.0018007 |
inclination: | 73.8694° |
perigee height: | 762 km |
apogee height: | 787 km |
right ascension of ascending node: | 132.8862° |
argument of perigee: | 231.5289° |
revolutions per day: | 14.35117057 |
mean anomaly at epoch: | 128.4248° |
orbit number at epoch: | 75936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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