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 17590U 87027B 22228.16632741 -.00000076 00000-0 -13919-4 0 9994
2 17590 71.0033 138.2926 0007030 296.1747 63.8653 14.16830132831018
Epoch (UTC): | 16 August 2022 03:59:30 |
Eccentricity: | 0.0007030 |
inclination: | 71.0033° |
perigee height: | 831 km |
apogee height: | 841 km |
right ascension of ascending node: | 138.2926° |
argument of perigee: | 296.1747° |
revolutions per day: | 14.16830132 |
mean anomaly at epoch: | 63.8653° |
orbit number at epoch: | 83101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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