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 33591U 09005A 19344.95174627 +.00000006 +00000-0 +28651-4 0 9999
2 33591 099.1909 340.4155 0013111 245.9449 114.0350 14.12386851558388
Epoch (UTC): | 10 December 2019 22:50:30 |
Eccentricity: | 0.0013111 |
inclination: | 99.1909° |
perigee height: | 842 km |
apogee height: | 860 km |
right ascension of ascending node: | 340.4155° |
argument of perigee: | 245.9449° |
revolutions per day: | 14.12386851 |
mean anomaly at epoch: | 114.0350° |
orbit number at epoch: | 55838 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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