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 17589U 26075.86845604 +.00000000 +00000-0 -87049-4 0 00007
2 17589 70.9206 310.9314 0023904 204.2910 155.7086 14.13052659 01
| Epoch (UTC): | 16 March 2026 20:50:34 |
| Eccentricity: | 0.0023904 |
| inclination: | 70.9206° |
| perigee height: | 832 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 310.9314° |
| argument of perigee: | 204.2910° |
| revolutions per day: | 14.13052659 |
| mean anomaly at epoch: | 155.7086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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