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 66231U 26145.63931178 +.00000000 +00000-0 +96132-3 0 00001
2 66231 53.1596 232.2829 0000707 91.9577 268.1505 15.30211214 06
| Epoch (UTC): | 25 May 2026 15:20:36 |
| Eccentricity: | 0.0000707 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.2829° |
| argument of perigee: | 91.9577° |
| revolutions per day: | 15.30211214 |
| mean anomaly at epoch: | 268.1505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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