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 43789U 18099AH 25138.74394592 .00035200 00000-0 99139-3 0 9994
2 43789 97.4659 206.3440 0009687 207.8184 152.2543 15.36324114353656
Epoch (UTC): | 18 May 2025 17:51:16 |
Eccentricity: | 0.0009687 |
inclination: | 97.4659° |
perigee height: | 450 km |
apogee height: | 463 km |
right ascension of ascending node: | 206.3440° |
argument of perigee: | 207.8184° |
revolutions per day: | 15.36324114 |
mean anomaly at epoch: | 152.2543° |
orbit number at epoch: | 35365 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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