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 37839U 11058B 24277.01535000 .00001514 00000-0 65448-3 0 9992
2 37839 19.9598 127.3455 0018685 46.8452 110.6847 14.13343850670997
Epoch (UTC): | 03 October 2024 00:22:06 |
Eccentricity: | 0.0018685 |
inclination: | 19.9598° |
perigee height: | 834 km |
apogee height: | 861 km |
right ascension of ascending node: | 127.3455° |
argument of perigee: | 46.8452° |
revolutions per day: | 14.13343850 |
mean anomaly at epoch: | 110.6847° |
orbit number at epoch: | 67099 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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