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 33498U 09002G 21023.58096328 .00000211 00000-0 35784-4 0 9992
2 33498 98.2344 260.3520 0012162 91.4286 268.8317 14.79264876646048
| Epoch (UTC): | 23 January 2021 13:56:35 |
| Eccentricity: | 0.0012162 |
| inclination: | 98.2344° |
| perigee height: | 623 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 260.3520° |
| argument of perigee: | 91.4286° |
| revolutions per day: | 14.79264876 |
| mean anomaly at epoch: | 268.8317° |
| orbit number at epoch: | 64604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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