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 66340U 26145.33912697 +.00000000 +00000-0 +35143-3 0 00009
2 66340 43.0006 139.9190 0001172 272.0597 88.0120 15.27581360 06
| Epoch (UTC): | 25 May 2026 08:08:20 |
| Eccentricity: | 0.0001172 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.9190° |
| argument of perigee: | 272.0597° |
| revolutions per day: | 15.27581360 |
| mean anomaly at epoch: | 88.0120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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