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 19324.22273677 -.00000108 00000-0 -20708-3 0 9996
2 50 47.2330 53.7516 0113036 59.3329 301.8546 12.20108722645016
| Epoch (UTC): | 20 November 2019 05:20:44 |
| Eccentricity: | 0.0113036 |
| inclination: | 47.2330° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 53.7516° |
| argument of perigee: | 59.3329° |
| revolutions per day: | 12.20108722 |
| mean anomaly at epoch: | 301.8546° |
| orbit number at epoch: | 64501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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