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 00050U 60009B 25341.22750660 -.00000045 00000-0 38311-3 0 9992
2 00050 47.2330 37.5561 0113785 163.1473 197.3142 12.20161665914262
| Epoch (UTC): | 07 December 2025 05:27:36 |
| Eccentricity: | 0.0113785 |
| inclination: | 47.2330° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 37.5561° |
| argument of perigee: | 163.1473° |
| revolutions per day: | 12.20161665 |
| mean anomaly at epoch: | 197.3142° |
| orbit number at epoch: | 91426 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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