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 15332U 84105B 24317.88109034 .00001337 00000-0 15325-3 0 9995
2 15332 82.5347 177.5445 0022008 83.2109 287.4856 14.85041253146692
Epoch (UTC): | 12 November 2024 21:08:46 |
Eccentricity: | 0.0022008 |
inclination: | 82.5347° |
perigee height: | 598 km |
apogee height: | 629 km |
right ascension of ascending node: | 177.5445° |
argument of perigee: | 83.2109° |
revolutions per day: | 14.85041253 |
mean anomaly at epoch: | 287.4856° |
orbit number at epoch: | 14669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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