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 39250U 13048B 19016.70386083 +.00000008 +00000-0 -13704-4 0 9995
2 39250 082.4831 232.3160 0018801 033.7901 326.4366 12.42930654242582
| Epoch (UTC): | 16 January 2019 16:53:33 |
| Eccentricity: | 0.0018801 |
| inclination: | 82.4831° |
| perigee height: | 1479 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 232.3160° |
| argument of perigee: | 33.7901° |
| revolutions per day: | 12.42930654 |
| mean anomaly at epoch: | 326.4366° |
| orbit number at epoch: | 24258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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