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 is defined by the following mean orbital elements,
1 43168U 18010F 18081.42604271 .28808768 -13411-5 35134-2 0 9997
2 43168 82.8880 78.1866 0005783 272.9878 87.6140 16.36378329 9474
| Epoch (UTC): | 22 March 2018 10:13:30 |
| Eccentricity: | 0.0005783 |
| inclination: | 82.8880° |
| perigee height: | 171 km |
| apogee height: | 179 km |
| right ascension of ascending node: | 78.1866° |
| argument of perigee: | 272.9878° |
| revolutions per day: | 16.36378329 |
| mean anomaly at epoch: | 87.6140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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