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 26063U 00004C 21064.72671505 .00000003 00000-0 20901-4 0 9996
2 26063 100.1897 339.0855 0037167 80.7607 279.7775 14.36780295106310
Epoch (UTC): | 05 March 2021 17:26:28 |
Eccentricity: | 0.0037167 |
inclination: | 100.1897° |
perigee height: | 742 km |
apogee height: | 796 km |
right ascension of ascending node: | 339.0855° |
argument of perigee: | 80.7607° |
revolutions per day: | 14.36780295 |
mean anomaly at epoch: | 279.7775° |
orbit number at epoch: | 10631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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