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 37852U 11061C 23083.64649024 .00057790 00000-0 19404-2 0 9993
2 37852 101.7062 6.1848 0117581 286.0217 72.8081 15.24186083624433
Epoch (UTC): | 24 March 2023 15:30:56 |
Eccentricity: | 0.0117581 |
inclination: | 101.7062° |
perigee height: | 412 km |
apogee height: | 574 km |
right ascension of ascending node: | 6.1848° |
argument of perigee: | 286.0217° |
revolutions per day: | 15.24186083 |
mean anomaly at epoch: | 72.8081° |
orbit number at epoch: | 62443 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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