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 43786U 18099AE 25138.65182903 .00007390 00000-0 42535-3 0 9999
2 43786 97.4572 193.4870 0012652 282.4625 77.5191 15.12660172353148
Epoch (UTC): | 18 May 2025 15:38:38 |
Eccentricity: | 0.0012652 |
inclination: | 97.4572° |
perigee height: | 519 km |
apogee height: | 537 km |
right ascension of ascending node: | 193.4870° |
argument of perigee: | 282.4625° |
revolutions per day: | 15.12660172 |
mean anomaly at epoch: | 77.5191° |
orbit number at epoch: | 35314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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