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 66656U 26144.75959373 +.00000000 +00000-0 +18989-3 0 00005
2 66656 97.7482 74.3441 0015422 77.1307 283.1635 14.93258433 00
| Epoch (UTC): | 24 May 2026 18:13:48 |
| Eccentricity: | 0.0015422 |
| inclination: | 97.7482° |
| perigee height: | 577 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 74.3441° |
| argument of perigee: | 77.1307° |
| revolutions per day: | 14.93258433 |
| mean anomaly at epoch: | 283.1635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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