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 19107.91343133 -.00000076 +00000-0 +96604-4 0 9998
2 50 047.2335 005.1016 0113315 134.3965 226.6168 12.20107577618142
| Epoch (UTC): | 17 April 2019 21:55:20 |
| Eccentricity: | 0.0113315 |
| inclination: | 47.2335° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 5.1016° |
| argument of perigee: | 134.3965° |
| revolutions per day: | 12.20107577 |
| mean anomaly at epoch: | 226.6168° |
| orbit number at epoch: | 61814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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