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 66470U 26145.57355441 +.00000000 +00000-0 +83783-3 0 00000
2 66470 42.9983 222.0688 0001472 273.1883 86.8800 15.27591004 08
| Epoch (UTC): | 25 May 2026 13:45:55 |
| Eccentricity: | 0.0001472 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.0688° |
| argument of perigee: | 273.1883° |
| revolutions per day: | 15.27591004 |
| mean anomaly at epoch: | 86.8800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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