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 42733U 98067MN 19073.81661424 .22721454 12576-4 28234-3 0 9995
2 42733 51.6021 29.3648 0005433 200.7020 239.9908 16.49371243103244
| Epoch (UTC): | 14 March 2019 19:35:55 |
| Eccentricity: | 0.0005433 |
| inclination: | 51.6021° |
| perigee height: | 137 km |
| apogee height: | 144 km |
| right ascension of ascending node: | 29.3648° |
| argument of perigee: | 200.7020° |
| revolutions per day: | 16.49371243 |
| mean anomaly at epoch: | 239.9908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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