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 39266U 13055B 23081.42686668 .00032798 00000-0 74594-3 0 9991
2 39266 80.9728 301.1931 0538648 106.9342 259.1611 14.59725792494585
Epoch (UTC): | 22 March 2023 10:14:41 |
Eccentricity: | 0.0538648 |
inclination: | 80.9728° |
perigee height: | 313 km |
apogee height: | 1075 km |
right ascension of ascending node: | 301.1931° |
argument of perigee: | 106.9342° |
revolutions per day: | 14.59725792 |
mean anomaly at epoch: | 259.1611° |
orbit number at epoch: | 49458 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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