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 42735U 98067MQ 19177.57459781 .06778492 12465-4 49079-3 0 9999
2 42735 51.6126 219.5412 0004976 324.5993 156.4142 16.39992869120917
| Epoch (UTC): | 26 June 2019 13:47:25 |
| Eccentricity: | 0.0004976 |
| inclination: | 51.6126° |
| perigee height: | 162 km |
| apogee height: | 169 km |
| right ascension of ascending node: | 219.5412° |
| argument of perigee: | 324.5993° |
| revolutions per day: | 16.39992869 |
| mean anomaly at epoch: | 156.4142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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