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 66480U 26145.57612513 +.00000000 +00000-0 +82309-3 0 00000
2 66480 42.9983 222.0818 0001565 273.9410 86.1263 15.27591384 08
| Epoch (UTC): | 25 May 2026 13:49:37 |
| Eccentricity: | 0.0001565 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.0818° |
| argument of perigee: | 273.9410° |
| revolutions per day: | 15.27591384 |
| mean anomaly at epoch: | 86.1263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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