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 58743U 26145.44456895 +.00000000 +00000-0 -27940-4 0 00000
2 58743 43.0037 146.1817 0001163 275.7942 84.2777 15.27571881 01
| Epoch (UTC): | 25 May 2026 10:40:10 |
| Eccentricity: | 0.0001163 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.1817° |
| argument of perigee: | 275.7942° |
| revolutions per day: | 15.27571881 |
| mean anomaly at epoch: | 84.2777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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