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 64326U 26145.44013105 +.00000000 +00000-0 +15352-2 0 00008
2 64326 43.0004 286.7277 0001869 260.3436 99.7220 15.70915366 03
| Epoch (UTC): | 25 May 2026 10:33:47 |
| Eccentricity: | 0.0001869 |
| inclination: | 43.0004° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 286.7277° |
| argument of perigee: | 260.3436° |
| revolutions per day: | 15.70915366 |
| mean anomaly at epoch: | 99.7220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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