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 59475U 26145.51515520 +.00000000 +00000-0 +80646-4 0 00003
2 59475 43.0018 320.5182 0001074 269.9154 90.1575 15.27569414 08
| Epoch (UTC): | 25 May 2026 12:21:49 |
| Eccentricity: | 0.0001074 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.5182° |
| argument of perigee: | 269.9154° |
| revolutions per day: | 15.27569414 |
| mean anomaly at epoch: | 90.1575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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