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 24797U 97020F 24306.44846381 .00002730 00000-0 56038-3 0 9997
2 24797 86.8910 85.8819 0217098 327.2250 89.5937 14.46527879446851
Epoch (UTC): | 01 November 2024 10:45:47 |
Eccentricity: | 0.0217098 |
inclination: | 86.8910° |
perigee height: | 582 km |
apogee height: | 891 km |
right ascension of ascending node: | 85.8819° |
argument of perigee: | 327.2250° |
revolutions per day: | 14.46527879 |
mean anomaly at epoch: | 89.5937° |
orbit number at epoch: | 44685 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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