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 22141.68970734 .00005118 00000-0 39028-3 0 9997
2 43017 97.6771 36.9730 0247603 275.5217 81.7804 14.81254382243154
Epoch (UTC): | 21 May 2022 16:33:10 |
Eccentricity: | 0.0247603 |
inclination: | 97.6771° |
perigee height: | 452 km |
apogee height: | 799 km |
right ascension of ascending node: | 36.9730° |
argument of perigee: | 275.5217° |
revolutions per day: | 14.81254382 |
mean anomaly at epoch: | 81.7804° |
orbit number at epoch: | 24315 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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