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 13514U 61015KX 24357.91313359 .00000474 00000-0 70161-3 0 9995
2 13514 66.7133 186.4547 0242862 12.9209 92.1805 13.50818449191441
Epoch (UTC): | 22 December 2024 21:54:54 |
Eccentricity: | 0.0242862 |
inclination: | 66.7133° |
perigee height: | 888 km |
apogee height: | 1250 km |
right ascension of ascending node: | 186.4547° |
argument of perigee: | 12.9209° |
revolutions per day: | 13.50818449 |
mean anomaly at epoch: | 92.1805° |
orbit number at epoch: | 19144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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