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 59742U 26145.37611896 +.00000000 +00000-0 +53396-4 0 00009
2 59742 43.0021 110.7884 0001073 255.0796 104.9937 15.27581613 05
| Epoch (UTC): | 25 May 2026 09:01:36 |
| Eccentricity: | 0.0001073 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.7884° |
| argument of perigee: | 255.0796° |
| revolutions per day: | 15.27581613 |
| mean anomaly at epoch: | 104.9937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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