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 25340.89990826 -.00000051 00000-0 32355-3 0 9993
2 00050 47.2330 38.5729 0113781 162.1700 198.3129 12.20161642914224
| Epoch (UTC): | 06 December 2025 21:35:52 |
| Eccentricity: | 0.0113781 |
| inclination: | 47.2330° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 38.5729° |
| argument of perigee: | 162.1700° |
| revolutions per day: | 12.20161642 |
| mean anomaly at epoch: | 198.3129° |
| orbit number at epoch: | 91422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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