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 66338U 26145.30957312 +.00000000 +00000-0 +51039-3 0 00008
2 66338 43.0019 139.7035 0002063 273.5117 86.5499 15.27590276 05
| Epoch (UTC): | 25 May 2026 07:25:47 |
| Eccentricity: | 0.0002063 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.7035° |
| argument of perigee: | 273.5117° |
| revolutions per day: | 15.27590276 |
| mean anomaly at epoch: | 86.5499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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