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 58827U 26145.43916874 +.00000000 +00000-0 +57987-3 0 00002
2 58827 53.1578 208.0586 0000999 72.9191 287.1919 15.30208422 00
| Epoch (UTC): | 25 May 2026 10:32:24 |
| Eccentricity: | 0.0000999 |
| inclination: | 53.1578° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 208.0586° |
| argument of perigee: | 72.9191° |
| revolutions per day: | 15.30208422 |
| mean anomaly at epoch: | 287.1919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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