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 42711U 98067LS 19341.54612871 .05047864 12404-4 48655-3 0 9997
2 42711 51.6131 104.3875 0007128 330.3172 29.7448 16.37525667146451
| Epoch (UTC): | 07 December 2019 13:06:25 |
| Eccentricity: | 0.0007128 |
| inclination: | 51.6131° |
| perigee height: | 168 km |
| apogee height: | 177 km |
| right ascension of ascending node: | 104.3875° |
| argument of perigee: | 330.3172° |
| revolutions per day: | 16.37525667 |
| mean anomaly at epoch: | 29.7448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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