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 66475U 26145.52230066 +.00000000 +00000-0 +71158-3 0 00008
2 66475 43.0015 222.5425 0001465 276.2514 83.8171 15.27592513 06
| Epoch (UTC): | 25 May 2026 12:32:06 |
| Eccentricity: | 0.0001465 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.5425° |
| argument of perigee: | 276.2514° |
| revolutions per day: | 15.27592513 |
| mean anomaly at epoch: | 83.8171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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