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 66945U 26145.32700348 +.00000000 +00000-0 +53241-3 0 00006
2 66945 53.1611 2.2356 0001814 100.5335 259.5872 15.34399558 08
| Epoch (UTC): | 25 May 2026 07:50:53 |
| Eccentricity: | 0.0001814 |
| inclination: | 53.1611° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 2.2356° |
| argument of perigee: | 100.5335° |
| revolutions per day: | 15.34399558 |
| mean anomaly at epoch: | 259.5872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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