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 1778U 65096A 18264.90429699 +.00000057 +00000-0 +21172-4 0 9997
2 1778 034.2543 182.3027 0751451 098.6987 269.9444 13.46882332583463
| Epoch (UTC): | 21 September 2018 21:42:11 |
| Eccentricity: | 0.0751451 |
| inclination: | 34.2543° |
| perigee height: | 523 km |
| apogee height: | 1644 km |
| right ascension of ascending node: | 182.3027° |
| argument of perigee: | 98.6987° |
| revolutions per day: | 13.46882332 |
| mean anomaly at epoch: | 269.9444° |
| orbit number at epoch: | 58346 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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