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 42713U 98067LU 19151.03730059 .02928871 12128-4 58594-3 0 9990
2 42713 51.6172 356.2792 0012791 275.7272 84.2292 16.30383675116521
| Epoch (UTC): | 31 May 2019 00:53:42 |
| Eccentricity: | 0.0012791 |
| inclination: | 51.6172° |
| perigee height: | 183 km |
| apogee height: | 200 km |
| right ascension of ascending node: | 356.2792° |
| argument of perigee: | 275.7272° |
| revolutions per day: | 16.30383675 |
| mean anomaly at epoch: | 84.2292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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