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 41765U 16057A 19200.28161137 .00235737 81559-5 15236-3 0 9993
2 41765 42.7846 135.0246 0143359 272.5645 218.4707 15.97835923162069
| Epoch (UTC): | 19 July 2019 06:45:31 |
| Eccentricity: | 0.0143359 |
| inclination: | 42.7846° |
| perigee height: | 185 km |
| apogee height: | 376 km |
| right ascension of ascending node: | 135.0246° |
| argument of perigee: | 272.5645° |
| revolutions per day: | 15.97835923 |
| mean anomaly at epoch: | 218.4707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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