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 17296.38101740 .00016717 00000-0 10270-3 0 9039
2 25544 51.6401 119.2683 0005168 44.4352 315.7214 15.54237005 1681
| Epoch (UTC): | 23 October 2017 09:08:39 |
| Eccentricity: | 0.0005168 |
| inclination: | 51.6401° |
| perigee height: | 401 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 119.2683° |
| argument of perigee: | 44.4352° |
| revolutions per day: | 15.54237005 |
| mean anomaly at epoch: | 315.7214° |
| orbit number at epoch: | 168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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