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 17526U 87017B 24287.28561440 .00000245 00000-0 23105-3 0 9992
2 17526 82.9047 200.6426 0041427 38.9893 321.4238 13.77107141874094
Epoch (UTC): | 13 October 2024 06:51:17 |
Eccentricity: | 0.0041427 |
inclination: | 82.9047° |
perigee height: | 944 km |
apogee height: | 1004 km |
right ascension of ascending node: | 200.6426° |
argument of perigee: | 38.9893° |
revolutions per day: | 13.77107141 |
mean anomaly at epoch: | 321.4238° |
orbit number at epoch: | 87409 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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