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 58488U 26144.97949543 +.00000000 +00000-0 +14804-4 0 00004
2 58488 43.0033 352.8117 0001471 255.9256 104.1432 15.27577931 04
| Epoch (UTC): | 24 May 2026 23:30:28 |
| Eccentricity: | 0.0001471 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.8117° |
| argument of perigee: | 255.9256° |
| revolutions per day: | 15.27577931 |
| mean anomaly at epoch: | 104.1432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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