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 59411U 26145.25218867 +.00000000 +00000-0 +43279-4 0 00009
2 59411 43.0055 343.9036 0001230 296.5149 63.5576 15.27576651 06
| Epoch (UTC): | 25 May 2026 06:03:09 |
| Eccentricity: | 0.0001230 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.9036° |
| argument of perigee: | 296.5149° |
| revolutions per day: | 15.27576651 |
| mean anomaly at epoch: | 63.5576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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