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 14558U 81053JN 22222.81234175 .00001681 00000-0 76272-3 0 9994
2 14558 82.9256 72.0248 0019318 173.2776 314.8533 14.21275214 92664
Epoch (UTC): | 10 August 2022 19:29:46 |
Eccentricity: | 0.0019318 |
inclination: | 82.9256° |
perigee height: | 807 km |
apogee height: | 835 km |
right ascension of ascending node: | 72.0248° |
argument of perigee: | 173.2776° |
revolutions per day: | 14.21275214 |
mean anomaly at epoch: | 314.8533° |
orbit number at epoch: | 9266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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