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 17973U 87041A 23161.26700996 .00000218 00000-0 13892-3 0 9996
2 17973 70.8998 350.0911 0029024 88.7072 271.7374 14.14230285861701
Epoch (UTC): | 10 June 2023 06:24:29 |
Eccentricity: | 0.0029024 |
inclination: | 70.8998° |
perigee height: | 824 km |
apogee height: | 866 km |
right ascension of ascending node: | 350.0911° |
argument of perigee: | 88.7072° |
revolutions per day: | 14.14230285 |
mean anomaly at epoch: | 271.7374° |
orbit number at epoch: | 86170 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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