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 24258.84141881 .00011226 00000-0 11163-2 0 9992
2 39417 97.7419 212.9229 0047364 221.3543 138.4086 14.90991943584932
Epoch (UTC): | 14 September 2024 20:11:38 |
Eccentricity: | 0.0047364 |
inclination: | 97.7419° |
perigee height: | 562 km |
apogee height: | 628 km |
right ascension of ascending node: | 212.9229° |
argument of perigee: | 221.3543° |
revolutions per day: | 14.90991943 |
mean anomaly at epoch: | 138.4086° |
orbit number at epoch: | 58493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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