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 is defined by the following mean orbital elements,
1 39392U 13064N 19299.59327166 .02006905 70739-5 69005-3 0 9995
2 39392 40.4759 8.4266 0006007 67.5900 292.5581 16.24361258335149
| Epoch (UTC): | 26 October 2019 14:14:18 |
| Eccentricity: | 0.0006007 |
| inclination: | 40.4759° |
| perigee height: | 204 km |
| apogee height: | 212 km |
| right ascension of ascending node: | 8.4266° |
| argument of perigee: | 67.5900° |
| revolutions per day: | 16.24361258 |
| mean anomaly at epoch: | 292.5581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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