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 33724U 99025DHM 23027.92411060 .00001001 00000-0 52393-3 0 9998
2 33724 98.6694 56.3995 0027990 324.9254 153.6693 14.16368379790845
Epoch (UTC): | 27 January 2023 22:10:43 |
Eccentricity: | 0.0027990 |
inclination: | 98.6694° |
perigee height: | 817 km |
apogee height: | 858 km |
right ascension of ascending node: | 56.3995° |
argument of perigee: | 324.9254° |
revolutions per day: | 14.16368379 |
mean anomaly at epoch: | 153.6693° |
orbit number at epoch: | 79084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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