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 54160C 22141D 23084.71993056 .00032822 00000-0 20578-2 0 849
2 54160 53.2165 137.2611 0001374 109.5891 119.9444 15.08812913 10
Epoch (UTC): | 25 March 2023 17:16:42 |
Eccentricity: | 0.0001374 |
inclination: | 53.2165° |
perigee height: | 539 km |
apogee height: | 541 km |
right ascension of ascending node: | 137.2611° |
argument of perigee: | 109.5891° |
revolutions per day: | 15.08812913 |
mean anomaly at epoch: | 119.9444° |
orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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