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 59614U 26145.53521843 +.00000000 +00000-0 +13179-3 0 00001
2 59614 43.0020 324.0584 0001306 269.4876 90.5826 15.27581058 06
| Epoch (UTC): | 25 May 2026 12:50:42 |
| Eccentricity: | 0.0001306 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.0584° |
| argument of perigee: | 269.4876° |
| revolutions per day: | 15.27581058 |
| mean anomaly at epoch: | 90.5826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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