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 19081.74738889 +.00000024 +00000-0 +10000-3 0 9992
2 39497 082.4884 016.8119 0018494 102.8332 257.4822 12.42678218237495
| Epoch (UTC): | 22 March 2019 17:56:14 |
| Eccentricity: | 0.0018494 |
| inclination: | 82.4884° |
| perigee height: | 1481 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 16.8119° |
| argument of perigee: | 102.8332° |
| revolutions per day: | 12.42678218 |
| mean anomaly at epoch: | 257.4822° |
| orbit number at epoch: | 23749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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