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 23333.74152125 .00013721 00000-0 91519-3 0 9996
2 43017 97.6032 211.6067 0222150 241.1912 116.6840 14.89137433325794
Epoch (UTC): | 29 November 2023 17:47:47 |
Eccentricity: | 0.0222150 |
inclination: | 97.6032° |
perigee height: | 445 km |
apogee height: | 755 km |
right ascension of ascending node: | 211.6067° |
argument of perigee: | 241.1912° |
revolutions per day: | 14.89137433 |
mean anomaly at epoch: | 116.6840° |
orbit number at epoch: | 32579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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