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 32791U 08021J 19345.75082462 .00000387 00000-0 44561-4 0 9991
2 32791 97.5322 343.3642 0013736 17.7426 342.4270 14.90929432630345
Epoch (UTC): | 11 December 2019 18:01:11 |
Eccentricity: | 0.0013736 |
inclination: | 97.5322° |
perigee height: | 585 km |
apogee height: | 604 km |
right ascension of ascending node: | 343.3642° |
argument of perigee: | 17.7426° |
revolutions per day: | 14.90929432 |
mean anomaly at epoch: | 342.4270° |
orbit number at epoch: | 63034 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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