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 43792U 18099AL 25138.69199164 .00002483 00000-0 19107-3 0 9994
2 43792 97.4463 187.1065 0011828 237.5101 122.4982 15.02517880352530
Epoch (UTC): | 18 May 2025 16:36:28 |
Eccentricity: | 0.0011828 |
inclination: | 97.4463° |
perigee height: | 551 km |
apogee height: | 567 km |
right ascension of ascending node: | 187.1065° |
argument of perigee: | 237.5101° |
revolutions per day: | 15.02517880 |
mean anomaly at epoch: | 122.4982° |
orbit number at epoch: | 35253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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