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 41935U 98067KX 18305.47522705 .06673673 12387-4 58971-3 0 9997
2 41935 51.6243 332.8723 0002264 27.6675 118.1989 16.38373561102788
| Epoch (UTC): | 01 November 2018 11:24:19 |
| Eccentricity: | 0.0002264 |
| inclination: | 51.6243° |
| perigee height: | 168 km |
| apogee height: | 171 km |
| right ascension of ascending node: | 332.8723° |
| argument of perigee: | 27.6675° |
| revolutions per day: | 16.38373561 |
| mean anomaly at epoch: | 118.1989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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