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 42724U 98067MD 18238.55288637 .32989438 12602-4 94761-3 0 9996
2 42724 51.6129 331.1144 0008406 301.9468 58.5777 16.44741502 71945
| Epoch (UTC): | 26 August 2018 13:16:09 |
| Eccentricity: | 0.0008406 |
| inclination: | 51.6129° |
| perigee height: | 148 km |
| apogee height: | 159 km |
| right ascension of ascending node: | 331.1144° |
| argument of perigee: | 301.9468° |
| revolutions per day: | 16.44741502 |
| mean anomaly at epoch: | 58.5777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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