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 66582U 26145.39278457 +.00000000 +00000-0 +60997-3 0 00007
2 66582 42.9995 273.6071 0001418 278.8184 81.2507 15.27587804 05
| Epoch (UTC): | 25 May 2026 09:25:36 |
| Eccentricity: | 0.0001418 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 273.6071° |
| argument of perigee: | 278.8184° |
| revolutions per day: | 15.27587804 |
| mean anomaly at epoch: | 81.2507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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