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 32785U 08021C 22178.43913867 .00001146 00000-0 12548-3 0 9992
2 32785 97.6576 148.9713 0012067 193.5440 166.5455 14.89622852767977
| Epoch (UTC): | 27 June 2022 10:32:21 |
| Eccentricity: | 0.0012067 |
| inclination: | 97.6576° |
| perigee height: | 590 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 148.9713° |
| argument of perigee: | 193.5440° |
| revolutions per day: | 14.89622852 |
| mean anomaly at epoch: | 166.5455° |
| orbit number at epoch: | 76797 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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