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 24357.81258052 .00009350 00000-0 87571-3 0 9990
2 39417 97.7588 310.3257 0044882 254.9499 104.6752 14.93505976599691
Epoch (UTC): | 22 December 2024 19:30:06 |
Eccentricity: | 0.0044882 |
inclination: | 97.7588° |
perigee height: | 556 km |
apogee height: | 618 km |
right ascension of ascending node: | 310.3257° |
argument of perigee: | 254.9499° |
revolutions per day: | 14.93505976 |
mean anomaly at epoch: | 104.6752° |
orbit number at epoch: | 59969 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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