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 59590U 26017.95181652 +.00000000 +00000-0 +57099-3 0 00007
2 59590 97.3255 33.4889 0350529 4.8871 355.5607 14.56723611 05
| Epoch (UTC): | 17 January 2026 22:50:36 |
| Eccentricity: | 0.0350529 |
| inclination: | 97.3255° |
| perigee height: | 456 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 33.4889° |
| argument of perigee: | 4.8871° |
| revolutions per day: | 14.56723611 |
| mean anomaly at epoch: | 355.5607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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