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 31904U 99025CLF 19199.26083448 .00001435 00000-0 10131-2 0 9997
2 31904 98.9226 5.0139 0182783 86.4909 275.7137 13.91736400611440
| Epoch (UTC): | 18 July 2019 06:15:36 |
| Eccentricity: | 0.0182783 |
| inclination: | 98.9226° |
| perigee height: | 789 km |
| apogee height: | 1056 km |
| right ascension of ascending node: | 5.0139° |
| argument of perigee: | 86.4909° |
| revolutions per day: | 13.91736400 |
| mean anomaly at epoch: | 275.7137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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