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 42701U 98067LJ 19078.69468843 .10049912 12420-4 43736-3 0 9992
2 42701 51.6203 2.9892 0006383 231.0998 128.9461 16.43161447105627
| Epoch (UTC): | 19 March 2019 16:40:21 |
| Eccentricity: | 0.0006383 |
| inclination: | 51.6203° |
| perigee height: | 153 km |
| apogee height: | 161 km |
| right ascension of ascending node: | 2.9892° |
| argument of perigee: | 231.0998° |
| revolutions per day: | 16.43161447 |
| mean anomaly at epoch: | 128.9461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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