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 66593U 26145.55470660 +.00000000 +00000-0 +46557-3 0 00003
2 66593 43.0002 341.8947 0001168 262.3416 97.7303 15.27593773 04
| Epoch (UTC): | 25 May 2026 13:18:46 |
| Eccentricity: | 0.0001168 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.8947° |
| argument of perigee: | 262.3416° |
| revolutions per day: | 15.27593773 |
| mean anomaly at epoch: | 97.7303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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