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 66330U 26145.46219525 +.00000000 +00000-0 +67775-3 0 00008
2 66330 42.9996 139.1290 0001749 263.8507 96.2145 15.27593679 07
| Epoch (UTC): | 25 May 2026 11:05:33 |
| Eccentricity: | 0.0001749 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.1290° |
| argument of perigee: | 263.8507° |
| revolutions per day: | 15.27593679 |
| mean anomaly at epoch: | 96.2145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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