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 58458U 26145.54624539 +.00000000 +00000-0 -63453-4 0 00005
2 58458 43.0043 327.1379 0001608 263.0039 97.0629 15.27553480 09
| Epoch (UTC): | 25 May 2026 13:06:35 |
| Eccentricity: | 0.0001608 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.1379° |
| argument of perigee: | 263.0039° |
| revolutions per day: | 15.27553480 |
| mean anomaly at epoch: | 97.0629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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