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 25317.15948428 .00003355 00000-0 19679-2 0 9997
2 12 32.8970 266.5391 1647547 41.2064 330.1847 11.48293997506489
| Epoch (UTC): | 13 November 2025 03:49:39 |
| Eccentricity: | 0.1647547 |
| inclination: | 32.8970° |
| perigee height: | 553 km |
| apogee height: | 3288 km |
| right ascension of ascending node: | 266.5391° |
| argument of perigee: | 41.2064° |
| revolutions per day: | 11.48293997 |
| mean anomaly at epoch: | 330.1847° |
| orbit number at epoch: | 50648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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