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 24279.84444235 .00017920 00000-0 17523-2 0 9997
2 39417 97.7468 233.5412 0049651 151.4028 208.9930 14.91458637588069
Epoch (UTC): | 05 October 2024 20:15:59 |
Eccentricity: | 0.0049651 |
inclination: | 97.7468° |
perigee height: | 559 km |
apogee height: | 628 km |
right ascension of ascending node: | 233.5412° |
argument of perigee: | 151.4028° |
revolutions per day: | 14.91458637 |
mean anomaly at epoch: | 208.9930° |
orbit number at epoch: | 58806 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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