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 39497U 13076E 18350.61766063 .00000024 00000-0 10000-3 0 9991
2 39497 82.4882 76.6962 0016519 316.5042 43.4730 12.42677543225556
| Epoch (UTC): | 16 December 2018 14:49:25 |
| Eccentricity: | 0.0016519 |
| inclination: | 82.4882° |
| perigee height: | 1482 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 76.6962° |
| argument of perigee: | 316.5042° |
| revolutions per day: | 12.42677543 |
| mean anomaly at epoch: | 43.4730° |
| orbit number at epoch: | 22555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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