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 19339.90338638 +.00000328 +00000-0 +89809-5 0 9991
2 20580 028.4679 166.3564 0002750 154.3976 346.4338 15.09308263426542
| Epoch (UTC): | 05 December 2019 21:40:52 |
| Eccentricity: | 0.0002750 |
| inclination: | 28.4679° |
| perigee height: | 536 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 166.3564° |
| argument of perigee: | 154.3976° |
| revolutions per day: | 15.09308263 |
| mean anomaly at epoch: | 346.4338° |
| orbit number at epoch: | 42654 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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