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 22177.58018179 .00000927 00000-0 12969-3 0 9994
2 33498 98.1685 69.7369 0009656 216.8679 143.1869 14.80014214722784
| Epoch (UTC): | 26 June 2022 13:55:27 |
| Eccentricity: | 0.0009656 |
| inclination: | 98.1685° |
| perigee height: | 622 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 69.7369° |
| argument of perigee: | 216.8679° |
| revolutions per day: | 14.80014214 |
| mean anomaly at epoch: | 143.1869° |
| orbit number at epoch: | 72278 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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