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 59782U 26145.33365517 +.00000000 +00000-0 +32230-4 0 00009
2 59782 43.0005 132.8469 0001229 275.7885 84.2826 15.27578790 05
| Epoch (UTC): | 25 May 2026 08:00:27 |
| Eccentricity: | 0.0001229 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.8469° |
| argument of perigee: | 275.7885° |
| revolutions per day: | 15.27578790 |
| mean anomaly at epoch: | 84.2826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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