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 66523U 26145.45014255 +.00000000 +00000-0 +46595-3 0 00001
2 66523 43.0022 204.3719 0000857 270.4166 89.6587 15.27587297 03
| Epoch (UTC): | 25 May 2026 10:48:12 |
| Eccentricity: | 0.0000857 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3719° |
| argument of perigee: | 270.4166° |
| revolutions per day: | 15.27587297 |
| mean anomaly at epoch: | 89.6587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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