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 66469U 26145.54014543 +.00000000 +00000-0 +35615-3 0 00001
2 66469 43.0033 221.8174 0001389 247.9030 112.1674 15.27586520 00
| Epoch (UTC): | 25 May 2026 12:57:48 |
| Eccentricity: | 0.0001389 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.8174° |
| argument of perigee: | 247.9030° |
| revolutions per day: | 15.27586520 |
| mean anomaly at epoch: | 112.1674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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