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 58596U 26145.47036294 +.00000000 +00000-0 +19665-3 0 00009
2 58596 43.0012 298.5172 0001335 275.4263 84.6436 15.27581928 09
| Epoch (UTC): | 25 May 2026 11:17:19 |
| Eccentricity: | 0.0001335 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 298.5172° |
| argument of perigee: | 275.4263° |
| revolutions per day: | 15.27581928 |
| mean anomaly at epoch: | 84.6436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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