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 32791U 08021J 22178.49816729 .00001719 00000-0 17165-3 0 9990
2 32791 97.6113 154.5114 0013483 149.3440 210.8570 14.92716373768777
| Epoch (UTC): | 27 June 2022 11:57:21 |
| Eccentricity: | 0.0013483 |
| inclination: | 97.6113° |
| perigee height: | 580 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 154.5114° |
| argument of perigee: | 149.3440° |
| revolutions per day: | 14.92716373 |
| mean anomaly at epoch: | 210.8570° |
| orbit number at epoch: | 76877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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