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 59659U 26145.49418003 +.00000000 +00000-0 -11194-3 0 00004
2 59659 43.0042 324.2216 0001012 245.5457 114.5290 15.27590263 07
| Epoch (UTC): | 25 May 2026 11:51:37 |
| Eccentricity: | 0.0001012 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.2216° |
| argument of perigee: | 245.5457° |
| revolutions per day: | 15.27590263 |
| mean anomaly at epoch: | 114.5290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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