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 39439U 13066Z 24281.41141858 .00057412 00000-0 37942-2 0 9999
2 39439 97.7233 244.5404 0042314 113.4742 247.0941 15.06420441588825
Epoch (UTC): | 07 October 2024 09:52:26 |
Eccentricity: | 0.0042314 |
inclination: | 97.7233° |
perigee height: | 518 km |
apogee height: | 576 km |
right ascension of ascending node: | 244.5404° |
argument of perigee: | 113.4742° |
revolutions per day: | 15.06420441 |
mean anomaly at epoch: | 247.0941° |
orbit number at epoch: | 58882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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