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 24197U 94029JY 24357.82522376 .00005957 00000-0 63371-3 0 9992
2 24197 82.0894 128.0324 0077495 293.2293 218.8280 14.86594886616177
Epoch (UTC): | 22 December 2024 19:48:19 |
Eccentricity: | 0.0077495 |
inclination: | 82.0894° |
perigee height: | 554 km |
apogee height: | 663 km |
right ascension of ascending node: | 128.0324° |
argument of perigee: | 293.2293° |
revolutions per day: | 14.86594886 |
mean anomaly at epoch: | 218.8280° |
orbit number at epoch: | 61617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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