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 43017U 17073E 23341.60292872 .00006537 00000-0 43673-3 0 9999
2 43017 97.6029 219.1706 0222232 214.9103 143.7372 14.89299911326965
Epoch (UTC): | 07 December 2023 14:28:13 |
Eccentricity: | 0.0222232 |
inclination: | 97.6029° |
perigee height: | 445 km |
apogee height: | 755 km |
right ascension of ascending node: | 219.1706° |
argument of perigee: | 214.9103° |
revolutions per day: | 14.89299911 |
mean anomaly at epoch: | 143.7372° |
orbit number at epoch: | 32696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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