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 50U 60009B 19169.42318446 -.00000091 00000-0 -53125-4 0 9990
2 50 47.2285 174.1985 0114287 317.4437 41.7539 12.20109370626101
| Epoch (UTC): | 18 June 2019 10:09:23 |
| Eccentricity: | 0.0114287 |
| inclination: | 47.2285° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 174.1985° |
| argument of perigee: | 317.4437° |
| revolutions per day: | 12.20109370 |
| mean anomaly at epoch: | 41.7539° |
| orbit number at epoch: | 62610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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