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 23336.63085232 .00011896 00000-0 79283-3 0 9996
2 43017 97.6034 214.3869 0221993 231.5347 126.5770 14.89220020326221
Epoch (UTC): | 02 December 2023 15:08:25 |
Eccentricity: | 0.0221993 |
inclination: | 97.6034° |
perigee height: | 445 km |
apogee height: | 755 km |
right ascension of ascending node: | 214.3869° |
argument of perigee: | 231.5347° |
revolutions per day: | 14.89220020 |
mean anomaly at epoch: | 126.5770° |
orbit number at epoch: | 32622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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