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 17325U 85056D 24357.39664030 .00002533 00000-0 21282-2 0 9994
2 17325 8.2872 35.8695 6351246 28.1192 355.0759 3.46134563350875
Epoch (UTC): | 22 December 2024 09:31:09 |
Eccentricity: | 0.6351246 |
inclination: | 8.2872° |
perigee height: | 357 km |
apogee height: | 23806 km |
right ascension of ascending node: | 35.8695° |
argument of perigee: | 28.1192° |
revolutions per day: | 3.46134563 |
mean anomaly at epoch: | 355.0759° |
orbit number at epoch: | 35087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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