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 37855U 11061F 22137.27035275 .00020817 00000-0 91903-3 0 9996
2 37855 101.7058 239.8876 0156212 155.9143 204.9480 15.11465902576997
Epoch (UTC): | 17 May 2022 06:29:18 |
Eccentricity: | 0.0156212 |
inclination: | 101.7058° |
perigee height: | 424 km |
apogee height: | 639 km |
right ascension of ascending node: | 239.8876° |
argument of perigee: | 155.9143° |
revolutions per day: | 15.11465902 |
mean anomaly at epoch: | 204.9480° |
orbit number at epoch: | 57699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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