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 04759U 70025DH 24356.84802427 .00001477 00000-0 16016-2 0 9999
2 04759 100.0237 326.1642 0001326 231.0233 193.9933 13.74859854720369
Epoch (UTC): | 21 December 2024 20:21:09 |
Eccentricity: | 0.0001326 |
inclination: | 100.0237° |
perigee height: | 981 km |
apogee height: | 983 km |
right ascension of ascending node: | 326.1642° |
argument of perigee: | 231.0233° |
revolutions per day: | 13.74859854 |
mean anomaly at epoch: | 193.9933° |
orbit number at epoch: | 72036 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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