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 18290.66877366 +.00000543 +00000-0 +22249-4 0 9998
2 20580 028.4706 025.3906 0002848 022.8705 091.0368 15.09113886363905
| Epoch (UTC): | 17 October 2018 16:03:02 |
| Eccentricity: | 0.0002848 |
| inclination: | 28.4706° |
| perigee height: | 537 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 25.3906° |
| argument of perigee: | 22.8705° |
| revolutions per day: | 15.09113886 |
| mean anomaly at epoch: | 91.0368° |
| orbit number at epoch: | 36390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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