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 23085.67249665 .00012049 00000-0 85725-3 0 9992
2 43017 97.6414 333.2846 0237098 341.9030 17.3848 14.84829253288933
Epoch (UTC): | 26 March 2023 16:08:23 |
Eccentricity: | 0.0237098 |
inclination: | 97.6414° |
perigee height: | 448 km |
apogee height: | 780 km |
right ascension of ascending node: | 333.2846° |
argument of perigee: | 341.9030° |
revolutions per day: | 14.84829253 |
mean anomaly at epoch: | 17.3848° |
orbit number at epoch: | 28893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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