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 59326U 26145.41788267 +.00000000 +00000-0 +42905-4 0 00003
2 59326 43.0019 124.9994 0001100 258.0342 102.0386 15.27579169 00
| Epoch (UTC): | 25 May 2026 10:01:45 |
| Eccentricity: | 0.0001100 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.9994° |
| argument of perigee: | 258.0342° |
| revolutions per day: | 15.27579169 |
| mean anomaly at epoch: | 102.0386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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