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 59675U 26145.53095449 +.00000000 +00000-0 +22949-3 0 00001
2 59675 43.0028 327.9527 0001355 284.0858 75.9843 15.27566707 07
| Epoch (UTC): | 25 May 2026 12:44:34 |
| Eccentricity: | 0.0001355 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.9527° |
| argument of perigee: | 284.0858° |
| revolutions per day: | 15.27566707 |
| mean anomaly at epoch: | 75.9843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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