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 58674U 26145.62415140 +.00000000 +00000-0 +22862-3 0 00007
2 58674 43.0061 10.5497 0001379 272.7481 87.3213 15.27588791 00
| Epoch (UTC): | 25 May 2026 14:58:46 |
| Eccentricity: | 0.0001379 |
| inclination: | 43.0061° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.5497° |
| argument of perigee: | 272.7481° |
| revolutions per day: | 15.27588791 |
| mean anomaly at epoch: | 87.3213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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