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 66332U 26145.37110860 +.00000000 +00000-0 +54743-3 0 00003
2 66332 43.0009 139.3054 0001266 268.6288 91.4419 15.27591011 08
| Epoch (UTC): | 25 May 2026 08:54:23 |
| Eccentricity: | 0.0001266 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.3054° |
| argument of perigee: | 268.6288° |
| revolutions per day: | 15.27591011 |
| mean anomaly at epoch: | 91.4419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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