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 66326U 26145.38652816 +.00000000 +00000-0 +74561-3 0 00009
2 66326 43.0025 139.4142 0001829 264.0017 96.0627 15.27601108 04
| Epoch (UTC): | 25 May 2026 09:16:36 |
| Eccentricity: | 0.0001829 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.4142° |
| argument of perigee: | 264.0017° |
| revolutions per day: | 15.27601108 |
| mean anomaly at epoch: | 96.0627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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