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 59588U 26048.25780550 +.00000000 +00000-0 +17483-1 0 00004
2 59588 97.2182 353.9633 0048015 136.6422 223.8535 13.88730917 05
| Epoch (UTC): | 17 February 2026 06:11:14 |
| Eccentricity: | 0.0048015 |
| inclination: | 97.2182° |
| perigee height: | 898 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 353.9633° |
| argument of perigee: | 136.6422° |
| revolutions per day: | 13.88730917 |
| mean anomaly at epoch: | 223.8535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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