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 59583U 26145.11829623 +.00000000 +00000-0 +61183-4 0 00006
2 59583 42.9994 297.1709 0001167 274.3858 85.6861 15.27575524 03
| Epoch (UTC): | 25 May 2026 02:50:20 |
| Eccentricity: | 0.0001167 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 297.1709° |
| argument of perigee: | 274.3858° |
| revolutions per day: | 15.27575524 |
| mean anomaly at epoch: | 85.6861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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