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 32785U 08021C 23078.79356699 .00006547 00000-0 65951-3 0 9991
2 32785 97.6962 46.7653 0013906 47.3661 312.8727 14.91409519807494
Epoch (UTC): | 19 March 2023 19:02:44 |
Eccentricity: | 0.0013906 |
inclination: | 97.6962° |
perigee height: | 584 km |
apogee height: | 603 km |
right ascension of ascending node: | 46.7653° |
argument of perigee: | 47.3661° |
revolutions per day: | 14.91409519 |
mean anomaly at epoch: | 312.8727° |
orbit number at epoch: | 80749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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