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 23159.45032681 .00000448 00000-0 96242-4 0 9997
2 37839 19.9590 175.9404 0019049 122.3929 30.2645 14.12960144602545
Epoch (UTC): | 08 June 2023 10:48:28 |
Eccentricity: | 0.0019049 |
inclination: | 19.9590° |
perigee height: | 835 km |
apogee height: | 863 km |
right ascension of ascending node: | 175.9404° |
argument of perigee: | 122.3929° |
revolutions per day: | 14.12960144 |
mean anomaly at epoch: | 30.2645° |
orbit number at epoch: | 60254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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