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 17360U 87009B 24357.58272309 .00000057 00000-0 41400-4 0 9993
2 17360 82.9191 21.3094 0033759 75.2102 43.0630 13.76967721903762
Epoch (UTC): | 22 December 2024 13:59:07 |
Eccentricity: | 0.0033759 |
inclination: | 82.9191° |
perigee height: | 950 km |
apogee height: | 999 km |
right ascension of ascending node: | 21.3094° |
argument of perigee: | 75.2102° |
revolutions per day: | 13.76967721 |
mean anomaly at epoch: | 43.0630° |
orbit number at epoch: | 90376 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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