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 43782U 18099AA 25139.13291584 .00008336 00000-0 45818-3 0 9993
2 43782 97.4606 194.3851 0011161 220.6999 139.3399 15.14290560353254
Epoch (UTC): | 19 May 2025 03:11:23 |
Eccentricity: | 0.0011161 |
inclination: | 97.4606° |
perigee height: | 515 km |
apogee height: | 531 km |
right ascension of ascending node: | 194.3851° |
argument of perigee: | 220.6999° |
revolutions per day: | 15.14290560 |
mean anomaly at epoch: | 139.3399° |
orbit number at epoch: | 35325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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