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 41789U 16059G 19341.44981465 .00000064 00000-0 21071-4 0 9994
2 41789 98.0485 39.4135 0028139 189.9261 170.1388 14.64281402170782
| Epoch (UTC): | 07 December 2019 10:47:43 |
| Eccentricity: | 0.0028139 |
| inclination: | 98.0485° |
| perigee height: | 659 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 39.4135° |
| argument of perigee: | 189.9261° |
| revolutions per day: | 14.64281402 |
| mean anomaly at epoch: | 170.1388° |
| orbit number at epoch: | 17078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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