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 58475U 26144.99184954 +.00000000 +00000-0 +11930-3 0 00005
2 58475 43.0039 356.3166 0001791 266.0088 94.0559 15.27575506 03
| Epoch (UTC): | 24 May 2026 23:48:15 |
| Eccentricity: | 0.0001791 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.3166° |
| argument of perigee: | 266.0088° |
| revolutions per day: | 15.27575506 |
| mean anomaly at epoch: | 94.0559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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