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 21798U 91082A 24315.88179507 .00000632 00000-0 33488-3 0 9997
2 21798 98.7542 343.9934 0013687 143.0867 217.1252 14.17173139702504
Epoch (UTC): | 10 November 2024 21:09:47 |
Eccentricity: | 0.0013687 |
inclination: | 98.7542° |
perigee height: | 825 km |
apogee height: | 845 km |
right ascension of ascending node: | 343.9934° |
argument of perigee: | 143.0867° |
revolutions per day: | 14.17173139 |
mean anomaly at epoch: | 217.1252° |
orbit number at epoch: | 70250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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