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 58017U 26145.49012044 +.00000000 +00000-0 +14126-3 0 00003
2 58017 97.8355 227.0437 0002345 120.9626 239.1823 14.91036663 02
| Epoch (UTC): | 25 May 2026 11:45:46 |
| Eccentricity: | 0.0002345 |
| inclination: | 97.8355° |
| perigee height: | 593 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 227.0437° |
| argument of perigee: | 120.9626° |
| revolutions per day: | 14.91036663 |
| mean anomaly at epoch: | 239.1823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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