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 19340.91049006 +.00000024 +00000-0 +10000-3 0 9995
2 39497 082.4876 215.3886 0016761 260.7337 099.1847 12.42682149269689
| Epoch (UTC): | 06 December 2019 21:51:06 |
| Eccentricity: | 0.0016761 |
| inclination: | 82.4876° |
| perigee height: | 1482 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 215.3886° |
| argument of perigee: | 260.7337° |
| revolutions per day: | 12.42682149 |
| mean anomaly at epoch: | 99.1847° |
| orbit number at epoch: | 26968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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