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 42910U 98067MZ 19293.66077481 .08093820 12441-4 64211-3 0 9992
2 42910 51.6167 353.5295 0003841 355.3485 137.8062 16.39261620124803
| Epoch (UTC): | 20 October 2019 15:51:30 |
| Eccentricity: | 0.0003841 |
| inclination: | 51.6167° |
| perigee height: | 165 km |
| apogee height: | 170 km |
| right ascension of ascending node: | 353.5295° |
| argument of perigee: | 355.3485° |
| revolutions per day: | 16.39261620 |
| mean anomaly at epoch: | 137.8062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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