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 58856U 26145.39095742 +.00000000 +00000-0 +42180-4 0 00001
2 58856 43.0018 175.6901 0001143 273.0001 87.0720 15.27578430 07
| Epoch (UTC): | 25 May 2026 09:22:58 |
| Eccentricity: | 0.0001143 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.6901° |
| argument of perigee: | 273.0001° |
| revolutions per day: | 15.27578430 |
| mean anomaly at epoch: | 87.0720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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