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 23090.65897120 .00013857 00000-0 98500-3 0 9994
2 43017 97.6418 338.0720 0236198 325.4344 33.1704 14.84958869289671
Epoch (UTC): | 31 March 2023 15:48:55 |
Eccentricity: | 0.0236198 |
inclination: | 97.6418° |
perigee height: | 448 km |
apogee height: | 779 km |
right ascension of ascending node: | 338.0720° |
argument of perigee: | 325.4344° |
revolutions per day: | 14.84958869 |
mean anomaly at epoch: | 33.1704° |
orbit number at epoch: | 28967 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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