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 39417U 13066B 23333.44014319 .00006832 00000-0 75475-3 0 9990
2 39417 97.7093 289.6723 0055085 102.8085 257.9294 14.86614577541732
Epoch (UTC): | 29 November 2023 10:33:48 |
Eccentricity: | 0.0055085 |
inclination: | 97.7093° |
perigee height: | 570 km |
apogee height: | 647 km |
right ascension of ascending node: | 289.6723° |
argument of perigee: | 102.8085° |
revolutions per day: | 14.86614577 |
mean anomaly at epoch: | 257.9294° |
orbit number at epoch: | 54173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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