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 66333U 26145.48146644 +.00000000 +00000-0 +51562-3 0 00001
2 66333 43.0004 139.2714 0001395 276.3748 83.6944 15.27595174 06
| Epoch (UTC): | 25 May 2026 11:33:18 |
| Eccentricity: | 0.0001395 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.2714° |
| argument of perigee: | 276.3748° |
| revolutions per day: | 15.27595174 |
| mean anomaly at epoch: | 83.6944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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