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 42911U 98067NA 19211.59990721 .12573504 12373-4 16975-3 0 9991
2 42911 51.5967 51.4643 0016837 210.2341 252.3102 16.47729788111909
| Epoch (UTC): | 30 July 2019 14:23:51 |
| Eccentricity: | 0.0016837 |
| inclination: | 51.5967° |
| perigee height: | 134 km |
| apogee height: | 156 km |
| right ascension of ascending node: | 51.4643° |
| argument of perigee: | 210.2341° |
| revolutions per day: | 16.47729788 |
| mean anomaly at epoch: | 252.3102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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