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 39439U 13066Z 19340.52943665 .00000373 00000-0 51843-4 0 9999
2 39439 97.5694 344.6245 0064988 192.7851 167.1718 14.81970601326241
| Epoch (UTC): | 06 December 2019 12:42:23 |
| Eccentricity: | 0.0064988 |
| inclination: | 97.5694° |
| perigee height: | 577 km |
| apogee height: | 668 km |
| right ascension of ascending node: | 344.6245° |
| argument of perigee: | 192.7851° |
| revolutions per day: | 14.81970601 |
| mean anomaly at epoch: | 167.1718° |
| orbit number at epoch: | 32624 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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