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 19200.87486041 -.00000088 +00000-0 -12291-4 0 9997
2 50 047.2324 076.5830 0113932 051.3921 309.7007 12.20109355629492
| Epoch (UTC): | 19 July 2019 20:59:47 |
| Eccentricity: | 0.0113932 |
| inclination: | 47.2324° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 76.5830° |
| argument of perigee: | 51.3921° |
| revolutions per day: | 12.20109355 |
| mean anomaly at epoch: | 309.7007° |
| orbit number at epoch: | 62949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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