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 41557U 16033B 23081.44531640 .00056683 00000-0 10449-2 0 9994
2 41557 97.3825 186.6099 0007953 104.8533 317.4918 15.48922843380151
Epoch (UTC): | 22 March 2023 10:41:15 |
Eccentricity: | 0.0007953 |
inclination: | 97.3825° |
perigee height: | 414 km |
apogee height: | 425 km |
right ascension of ascending node: | 186.6099° |
argument of perigee: | 104.8533° |
revolutions per day: | 15.48922843 |
mean anomaly at epoch: | 317.4918° |
orbit number at epoch: | 38015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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