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 12U 59001B 25338.64081690 .00001834 00000-0 10654-2 0 9997
2 12 32.8946 190.8521 1647171 154.9313 214.1287 11.48366657508955
| Epoch (UTC): | 04 December 2025 15:22:46 |
| Eccentricity: | 0.1647171 |
| inclination: | 32.8946° |
| perigee height: | 554 km |
| apogee height: | 3287 km |
| right ascension of ascending node: | 190.8521° |
| argument of perigee: | 154.9313° |
| revolutions per day: | 11.48366657 |
| mean anomaly at epoch: | 214.1287° |
| orbit number at epoch: | 50895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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