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 66224U 26145.62148841 +.00000000 +00000-0 +55657-3 0 00006
2 66224 53.1596 232.8881 0000730 81.3839 278.7245 15.30240211 09
| Epoch (UTC): | 25 May 2026 14:54:56 |
| Eccentricity: | 0.0000730 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.8881° |
| argument of perigee: | 81.3839° |
| revolutions per day: | 15.30240211 |
| mean anomaly at epoch: | 278.7245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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