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 58403U 26145.59114900 +.00000000 +00000-0 +24107-3 0 00007
2 58403 43.0038 338.5543 0001918 267.1264 92.9368 15.27553230 08
| Epoch (UTC): | 25 May 2026 14:11:15 |
| Eccentricity: | 0.0001918 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.5543° |
| argument of perigee: | 267.1264° |
| revolutions per day: | 15.27553230 |
| mean anomaly at epoch: | 92.9368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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