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 59368U 26145.58190583 +.00000000 +00000-0 +64051-4 0 00001
2 59368 43.0012 185.5091 0001396 271.1049 88.9642 15.27582577 01
| Epoch (UTC): | 25 May 2026 13:57:56 |
| Eccentricity: | 0.0001396 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.5091° |
| argument of perigee: | 271.1049° |
| revolutions per day: | 15.27582577 |
| mean anomaly at epoch: | 88.9642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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