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 66346U 26145.36853608 +.00000000 +00000-0 +55215-3 0 00006
2 66346 43.0020 139.2830 0001483 283.1882 76.8804 15.27588668 09
| Epoch (UTC): | 25 May 2026 08:50:41 |
| Eccentricity: | 0.0001483 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.2830° |
| argument of perigee: | 283.1882° |
| revolutions per day: | 15.27588668 |
| mean anomaly at epoch: | 76.8804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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