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 22826U 93061D 22220.36616414 .00000060 00000-0 40974-4 0 9992
2 22826 98.8787 252.3697 0007982 243.7957 116.2404 14.30531787505834
Epoch (UTC): | 08 August 2022 08:47:16 |
Eccentricity: | 0.0007982 |
inclination: | 98.8787° |
perigee height: | 784 km |
apogee height: | 795 km |
right ascension of ascending node: | 252.3697° |
argument of perigee: | 243.7957° |
revolutions per day: | 14.30531787 |
mean anomaly at epoch: | 116.2404° |
orbit number at epoch: | 50583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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