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 17296U 87003B 24281.82093091 .00002722 00000-0 31757-3 0 9991
2 17296 82.5308 46.9861 0019613 58.5733 301.7397 14.84732903 38910
Epoch (UTC): | 07 October 2024 19:42:08 |
Eccentricity: | 0.0019613 |
inclination: | 82.5308° |
perigee height: | 601 km |
apogee height: | 628 km |
right ascension of ascending node: | 46.9861° |
argument of perigee: | 58.5733° |
revolutions per day: | 14.84732903 |
mean anomaly at epoch: | 301.7397° |
orbit number at epoch: | 3891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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