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 66336U 26145.31085742 +.00000000 +00000-0 +44738-3 0 00004
2 66336 43.0015 139.7060 0001701 279.8749 80.1911 15.27589690 02
| Epoch (UTC): | 25 May 2026 07:27:38 |
| Eccentricity: | 0.0001701 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.7060° |
| argument of perigee: | 279.8749° |
| revolutions per day: | 15.27589690 |
| mean anomaly at epoch: | 80.1911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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