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 37932U 11068C 22228.82688120 .00000055 00000-0 44656-4 0 9990
2 37932 98.7238 164.7261 0036744 340.8523 31.5969 14.22151362557387
Epoch (UTC): | 16 August 2022 19:50:42 |
Eccentricity: | 0.0036744 |
inclination: | 98.7238° |
perigee height: | 791 km |
apogee height: | 844 km |
right ascension of ascending node: | 164.7261° |
argument of perigee: | 340.8523° |
revolutions per day: | 14.22151362 |
mean anomaly at epoch: | 31.5969° |
orbit number at epoch: | 55738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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