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 66596U 26145.59454418 +.00000000 +00000-0 +59739-3 0 00009
2 66596 43.0032 342.1987 0001075 269.1478 90.9251 15.27587621 00
| Epoch (UTC): | 25 May 2026 14:16:08 |
| Eccentricity: | 0.0001075 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.1987° |
| argument of perigee: | 269.1478° |
| revolutions per day: | 15.27587621 |
| mean anomaly at epoch: | 90.9251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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