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 42708U 98067LR 19057.60728726 .12539676 12620-4 24972-3 0 9992
2 42708 51.6043 110.2979 0003995 293.2873 66.7735 16.46993420102181
| Epoch (UTC): | 26 February 2019 14:34:29 |
| Eccentricity: | 0.0003995 |
| inclination: | 51.6043° |
| perigee height: | 144 km |
| apogee height: | 150 km |
| right ascension of ascending node: | 110.2979° |
| argument of perigee: | 293.2873° |
| revolutions per day: | 16.46993420 |
| mean anomaly at epoch: | 66.7735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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