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 25544U 98067A 24310.56599976 .00027907 00000-0 47388-3 0 9994
2 25544 51.6413 335.0277 0009023 139.6035 356.4851 15.51208836480474
Epoch (UTC): | 05 November 2024 13:35:02 |
Eccentricity: | 0.0009023 |
inclination: | 51.6413° |
perigee height: | 407 km |
apogee height: | 419 km |
right ascension of ascending node: | 335.0277° |
argument of perigee: | 139.6035° |
revolutions per day: | 15.51208836 |
mean anomaly at epoch: | 356.4851° |
orbit number at epoch: | 48047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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