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 42912U 98067NB 19248.70315973 .02500102 12117-4 52303-3 0 9999
2 42912 51.6267 222.5515 0001059 185.4160 169.3834 16.30208236117744
| Epoch (UTC): | 05 September 2019 16:52:33 |
| Eccentricity: | 0.0001059 |
| inclination: | 51.6267° |
| perigee height: | 191 km |
| apogee height: | 192 km |
| right ascension of ascending node: | 222.5515° |
| argument of perigee: | 185.4160° |
| revolutions per day: | 16.30208236 |
| mean anomaly at epoch: | 169.3834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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