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 23083.42542268 -.00000076 00000-0 94806-4 0 9994
2 50 47.2293 226.6332 0113706 95.9983 265.3777 12.20128210793992
| Epoch (UTC): | 24 March 2023 10:12:36 |
| Eccentricity: | 0.0113706 |
| inclination: | 47.2293° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 226.6332° |
| argument of perigee: | 95.9983° |
| revolutions per day: | 12.20128210 |
| mean anomaly at epoch: | 265.3777° |
| orbit number at epoch: | 79399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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