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 data is extracted from the following two-line orbital elements,
1 25544U 98067A 19289.88037037 .00000199 00000-0 11467-4 0 9997
2 25544 51.6427 117.8307 0007115 154.9454 50.6676 15.50199420194134
| Epoch (UTC): | 16 October 2019 21:07:44 |
| Eccentricity: | 0.0007115 |
| inclination: | 51.6427° |
| perigee height: | 411 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 117.8307° |
| argument of perigee: | 154.9454° |
| revolutions per day: | 15.50199420 |
| mean anomaly at epoch: | 50.6676° |
| orbit number at epoch: | 19413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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