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 37791U 11044D 24260.20157556 .00002267 00000-0 41465-3 0 9992
2 37791 98.0772 350.2765 0022169 58.4294 356.9741 14.66679277699488
Epoch (UTC): | 16 September 2024 04:50:16 |
Eccentricity: | 0.0022169 |
inclination: | 98.0772° |
perigee height: | 656 km |
apogee height: | 687 km |
right ascension of ascending node: | 350.2765° |
argument of perigee: | 58.4294° |
revolutions per day: | 14.66679277 |
mean anomaly at epoch: | 356.9741° |
orbit number at epoch: | 69948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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