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 19144.60611350 -.00000012 +00000-0 +67875-3 0 9991
2 50 047.2312 251.2211 0114156 243.6409 115.2621 12.20108772622622
| Epoch (UTC): | 24 May 2019 14:32:48 |
| Eccentricity: | 0.0114156 |
| inclination: | 47.2312° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 251.2211° |
| argument of perigee: | 243.6409° |
| revolutions per day: | 12.20108772 |
| mean anomaly at epoch: | 115.2621° |
| orbit number at epoch: | 62262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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