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 66432U 26145.51595252 +.00000000 +00000-0 +80034-4 0 00005
2 66432 42.9990 200.2326 0001623 276.3103 83.7563 15.27566635 03
| Epoch (UTC): | 25 May 2026 12:22:58 |
| Eccentricity: | 0.0001623 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.2326° |
| argument of perigee: | 276.3103° |
| revolutions per day: | 15.27566635 |
| mean anomaly at epoch: | 83.7563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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