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 14547U 83120B 23342.49294521 .00000135 00000-0 11933-3 0 9994
2 14547 82.9299 130.6923 0047935 86.6921 273.9718 13.77244940765754
Epoch (UTC): | 08 December 2023 11:49:50 |
Eccentricity: | 0.0047935 |
inclination: | 82.9299° |
perigee height: | 938 km |
apogee height: | 1009 km |
right ascension of ascending node: | 130.6923° |
argument of perigee: | 86.6921° |
revolutions per day: | 13.77244940 |
mean anomaly at epoch: | 273.9718° |
orbit number at epoch: | 76575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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