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 is defined by the following mean orbital elements,
1 59539U 26145.38946962 +.00000000 +00000-0 -87201-5 0 00003
2 59539 43.0019 270.4444 0001221 273.5881 86.4831 15.27569685 09
| Epoch (UTC): | 25 May 2026 09:20:50 |
| Eccentricity: | 0.0001221 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.4444° |
| argument of perigee: | 273.5881° |
| revolutions per day: | 15.27569685 |
| mean anomaly at epoch: | 86.4831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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