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 22225.08489603 .00000139 00000-0 10034-3 0 9990
2 33591 99.1447 260.4017 0014381 32.9939 327.2126 14.12597749696440
| Epoch (UTC): | 13 August 2022 02:02:15 |
| Eccentricity: | 0.0014381 |
| inclination: | 99.1447° |
| perigee height: | 840 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 260.4017° |
| argument of perigee: | 32.9939° |
| revolutions per day: | 14.12597749 |
| mean anomaly at epoch: | 327.2126° |
| orbit number at epoch: | 69644 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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