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 39440U 13066AA 23340.41970880 .00003061 00000-0 38363-3 0 9991
2 39440 97.7928 283.8846 0072545 185.1841 174.8629 14.81083062539630
Epoch (UTC): | 06 December 2023 10:04:22 |
Eccentricity: | 0.0072545 |
inclination: | 97.7928° |
perigee height: | 575 km |
apogee height: | 677 km |
right ascension of ascending node: | 283.8846° |
argument of perigee: | 185.1841° |
revolutions per day: | 14.81083062 |
mean anomaly at epoch: | 174.8629° |
orbit number at epoch: | 53963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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