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 35684U 09041D 18232.46952637 .00000042 00000-0 13088-4 0 9998
2 35684 98.1788 185.6794 0047805 154.2898 206.0704 14.79146356488588
| Epoch (UTC): | 20 August 2018 11:16:07 |
| Eccentricity: | 0.0047805 |
| inclination: | 98.1788° |
| perigee height: | 598 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 185.6794° |
| argument of perigee: | 154.2898° |
| revolutions per day: | 14.79146356 |
| mean anomaly at epoch: | 206.0704° |
| orbit number at epoch: | 48858 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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