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 38341U 12025E 22144.14532979 .00001902 00000-0 22603-3 0 9990
2 38341 98.5081 357.7973 0055783 124.1227 236.5295 14.84674483542125
Epoch (UTC): | 24 May 2022 03:29:16 |
Eccentricity: | 0.0055783 |
inclination: | 98.5081° |
perigee height: | 575 km |
apogee height: | 653 km |
right ascension of ascending node: | 357.7973° |
argument of perigee: | 124.1227° |
revolutions per day: | 14.84674483 |
mean anomaly at epoch: | 236.5295° |
orbit number at epoch: | 54212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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