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 19321.68368012 -.00000117 +00000-0 -28866-3 0 9994
2 50 047.2327 061.6317 0113063 051.7635 309.3268 12.20108846644240
| Epoch (UTC): | 17 November 2019 16:24:29 |
| Eccentricity: | 0.0113063 |
| inclination: | 47.2327° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 61.6317° |
| argument of perigee: | 51.7635° |
| revolutions per day: | 12.20108846 |
| mean anomaly at epoch: | 309.3268° |
| orbit number at epoch: | 64424 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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