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 41938U 17004B 19323.31558494 .49795426 -15199-4 51623-3 0 9990
2 41938 22.4917 300.6724 0180312 315.5236 85.8378 16.17663239 46816
| Epoch (UTC): | 19 November 2019 07:34:26 |
| Eccentricity: | 0.0180312 |
| inclination: | 22.4917° |
| perigee height: | 107 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 300.6724° |
| argument of perigee: | 315.5236° |
| revolutions per day: | 16.17663239 |
| mean anomaly at epoch: | 85.8378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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