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 17590U 26065.02189145 +.00000000 +00000-0 -44721-4 0 00007
2 17590 71.0014 284.2247 0003586 150.8635 209.2690 14.17165768 00
| Epoch (UTC): | 06 March 2026 00:31:31 |
| Eccentricity: | 0.0003586 |
| inclination: | 71.0014° |
| perigee height: | 832 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 284.2247° |
| argument of perigee: | 150.8635° |
| revolutions per day: | 14.17165768 |
| mean anomaly at epoch: | 209.2690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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