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 20U 59007A 18110.42831608 +.00000191 +00000-0 +84323-4 0 9991
2 20 033.3412 112.6762 1667692 041.6203 329.9979 11.55568982139302
| Epoch (UTC): | 20 April 2018 10:16:46 |
| Eccentricity: | 0.1667692 |
| inclination: | 33.3412° |
| perigee height: | 508 km |
| apogee height: | 3264 km |
| right ascension of ascending node: | 112.6762° |
| argument of perigee: | 41.6203° |
| revolutions per day: | 11.55568982 |
| mean anomaly at epoch: | 329.9979° |
| orbit number at epoch: | 13930 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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