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 19340.76026203 +.00000326 +00000-0 +88359-5 0 9996
2 20580 028.4680 160.6893 0002717 163.4166 322.4853 15.09308510426676
| Epoch (UTC): | 06 December 2019 18:14:46 |
| Eccentricity: | 0.0002717 |
| inclination: | 28.4680° |
| perigee height: | 536 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 160.6893° |
| argument of perigee: | 163.4166° |
| revolutions per day: | 15.09308510 |
| mean anomaly at epoch: | 322.4853° |
| orbit number at epoch: | 42667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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