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 59610U 26145.47802708 +.00000000 +00000-0 +34173-4 0 00000
2 59610 43.0045 321.0303 0001924 259.8419 100.2216 15.27571020 07
| Epoch (UTC): | 25 May 2026 11:28:21 |
| Eccentricity: | 0.0001924 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 321.0303° |
| argument of perigee: | 259.8419° |
| revolutions per day: | 15.27571020 |
| mean anomaly at epoch: | 100.2216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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