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 22081U 92053B 23031.12740714 .00000163 00000-0 67524-4 0 9995
2 22081 74.0444 284.0067 0034829 111.1003 249.3878 14.33717968592677
Epoch (UTC): | 31 January 2023 03:03:27 |
Eccentricity: | 0.0034829 |
inclination: | 74.0444° |
perigee height: | 754 km |
apogee height: | 804 km |
right ascension of ascending node: | 284.0067° |
argument of perigee: | 111.1003° |
revolutions per day: | 14.33717968 |
mean anomaly at epoch: | 249.3878° |
orbit number at epoch: | 59267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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