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 66331U 26145.36082681 +.00000000 +00000-0 +48967-3 0 00001
2 66331 42.9999 139.2208 0001419 259.1552 100.9140 15.27585828 08
| Epoch (UTC): | 25 May 2026 08:39:35 |
| Eccentricity: | 0.0001419 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.2208° |
| argument of perigee: | 259.1552° |
| revolutions per day: | 15.27585828 |
| mean anomaly at epoch: | 100.9140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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