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 10962U 78063B 23151.72909244 .00000125 00000-0 46484-4 0 9999
2 10962 74.0772 163.6773 0026060 228.3996 131.4927 14.41595456358943
Epoch (UTC): | 31 May 2023 17:29:53 |
Eccentricity: | 0.0026060 |
inclination: | 74.0772° |
perigee height: | 734 km |
apogee height: | 772 km |
right ascension of ascending node: | 163.6773° |
argument of perigee: | 228.3996° |
revolutions per day: | 14.41595456 |
mean anomaly at epoch: | 131.4927° |
orbit number at epoch: | 35894 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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