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 18344.81646045 +.00000225 +00000-0 +28238-4 0 9993
2 32791 097.5304 354.2709 0014266 145.2423 214.9731 14.90689825575749
| Epoch (UTC): | 10 December 2018 19:35:42 |
| Eccentricity: | 0.0014266 |
| inclination: | 97.5304° |
| perigee height: | 586 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 354.2709° |
| argument of perigee: | 145.2423° |
| revolutions per day: | 14.90689825 |
| mean anomaly at epoch: | 214.9731° |
| orbit number at epoch: | 57574 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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