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 39057U 13001A 23083.78710024 .00000045 00000-0 25413-3 0 9991
2 39057 82.4966 234.6838 0028209 80.8410 279.5854 12.42935993462141
Epoch (UTC): | 24 March 2023 18:53:25 |
Eccentricity: | 0.0028209 |
inclination: | 82.4966° |
perigee height: | 1472 km |
apogee height: | 1516 km |
right ascension of ascending node: | 234.6838° |
argument of perigee: | 80.8410° |
revolutions per day: | 12.42935993 |
mean anomaly at epoch: | 279.5854° |
orbit number at epoch: | 46214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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