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 18422U 87088B 22229.03503826 .00000288 00000-0 32314-4 0 9997
2 18422 82.5108 208.5159 0019124 348.3234 11.7534 14.83233602881467
Epoch (UTC): | 17 August 2022 00:50:27 |
Eccentricity: | 0.0019124 |
inclination: | 82.5108° |
perigee height: | 606 km |
apogee height: | 632 km |
right ascension of ascending node: | 208.5159° |
argument of perigee: | 348.3234° |
revolutions per day: | 14.83233602 |
mean anomaly at epoch: | 11.7534° |
orbit number at epoch: | 88146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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