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 20580U 90037B 17206.19286677 +.00000421 +00000-0 +14883-4 0 9991
2 20580 028.4697 116.3794 0002663 218.5634 275.8232 15.08803621295942
| Epoch (UTC): | 25 July 2017 04:37:43 |
| Eccentricity: | 0.0002663 |
| inclination: | 28.4697° |
| perigee height: | 538 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 116.3794° |
| argument of perigee: | 218.5634° |
| revolutions per day: | 15.08803621 |
| mean anomaly at epoch: | 275.8232° |
| orbit number at epoch: | 29594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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