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 20580U 90037B 24310.57024183 .00014545 00000-0 63113-3 0 9990
2 20580 28.4661 115.9533 0002687 126.5479 233.5362 15.20843224698556
Epoch (UTC): | 05 November 2024 13:41:08 |
Eccentricity: | 0.0002687 |
inclination: | 28.4661° |
perigee height: | 501 km |
apogee height: | 505 km |
right ascension of ascending node: | 115.9533° |
argument of perigee: | 126.5479° |
revolutions per day: | 15.20843224 |
mean anomaly at epoch: | 233.5362° |
orbit number at epoch: | 69855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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