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 58423U 26145.55901737 +.00000000 +00000-0 +29339-3 0 00009
2 58423 43.0054 338.2513 0001634 270.0379 90.0286 15.27555093 04
| Epoch (UTC): | 25 May 2026 13:24:59 |
| Eccentricity: | 0.0001634 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.2513° |
| argument of perigee: | 270.0379° |
| revolutions per day: | 15.27555093 |
| mean anomaly at epoch: | 90.0286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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