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 18266.78886499 .00016717 00000-0 10270-3 0 9032
2 25544 51.6400 247.3426 0003904 202.7723 157.3257 15.53758719 13842
| Epoch (UTC): | 23 September 2018 18:55:57 |
| Eccentricity: | 0.0003904 |
| inclination: | 51.6400° |
| perigee height: | 403 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 247.3426° |
| argument of perigee: | 202.7723° |
| revolutions per day: | 15.53758719 |
| mean anomaly at epoch: | 157.3257° |
| orbit number at epoch: | 1384 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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