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 18115.53706485 .00016717 00000-0 10270-3 0 9023
2 25544 51.6362 281.1814 0002748 9.6810 350.4395 15.54170842 30329
| Epoch (UTC): | 25 April 2018 12:53:22 |
| Eccentricity: | 0.0002748 |
| inclination: | 51.6362° |
| perigee height: | 403 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 281.1814° |
| argument of perigee: | 9.6810° |
| revolutions per day: | 15.54170842 |
| mean anomaly at epoch: | 350.4395° |
| orbit number at epoch: | 3032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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