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 25343.59572668 .00001803 00000-0 10402-2 0 9994
2 12 32.8961 173.3881 1647198 181.1757 178.4580 11.48383148509526
| Epoch (UTC): | 09 December 2025 14:17:50 |
| Eccentricity: | 0.1647198 |
| inclination: | 32.8961° |
| perigee height: | 553 km |
| apogee height: | 3287 km |
| right ascension of ascending node: | 173.3881° |
| argument of perigee: | 181.1757° |
| revolutions per day: | 11.48383148 |
| mean anomaly at epoch: | 178.4580° |
| orbit number at epoch: | 50952 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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