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 59566U 26145.44265381 +.00000000 +00000-0 +10993-3 0 00000
2 59566 42.9998 295.3157 0001279 278.2692 81.8015 15.27574466 01
| Epoch (UTC): | 25 May 2026 10:37:25 |
| Eccentricity: | 0.0001279 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.3157° |
| argument of perigee: | 278.2692° |
| revolutions per day: | 15.27574466 |
| mean anomaly at epoch: | 81.8015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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