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 19287.11960789 -.00000093 00000-0 -80641-4 0 9995
2 50 47.2307 168.9094 0113835 308.7728 50.2936 12.20109228640476
| Epoch (UTC): | 14 October 2019 02:52:14 |
| Eccentricity: | 0.0113835 |
| inclination: | 47.2307° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 168.9094° |
| argument of perigee: | 308.7728° |
| revolutions per day: | 12.20109228 |
| mean anomaly at epoch: | 50.2936° |
| orbit number at epoch: | 64047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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