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 25174.47720514 -.00000095 00000-0 -80214-4 0 9994
2 50 47.2286 195.1406 0112933 25.4306 335.1984 12.20156422894369
| Epoch (UTC): | 23 June 2025 11:27:10 |
| Eccentricity: | 0.0112933 |
| inclination: | 47.2286° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 195.1406° |
| argument of perigee: | 25.4306° |
| revolutions per day: | 12.20156422 |
| mean anomaly at epoch: | 335.1984° |
| orbit number at epoch: | 89436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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