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 21334.91497059 .00000462 00000-0 69159-4 0 9991
2 33498 98.1900 218.3360 0010990 164.3728 195.7824 14.79500131692070
| Epoch (UTC): | 30 November 2021 21:57:33 |
| Eccentricity: | 0.0010990 |
| inclination: | 98.1900° |
| perigee height: | 623 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 218.3360° |
| argument of perigee: | 164.3728° |
| revolutions per day: | 14.79500131 |
| mean anomaly at epoch: | 195.7824° |
| orbit number at epoch: | 69207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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