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 22182.65075638 .00000529 00000-0 77115-4 0 9994
2 33498 98.1676 74.8930 0010000 199.2419 160.8416 14.80021607723538
| Epoch (UTC): | 01 July 2022 15:37:05 |
| Eccentricity: | 0.0010000 |
| inclination: | 98.1676° |
| perigee height: | 622 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 74.8930° |
| argument of perigee: | 199.2419° |
| revolutions per day: | 14.80021607 |
| mean anomaly at epoch: | 160.8416° |
| orbit number at epoch: | 72353 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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