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 26137.72374691 +.00000000 +00000-0 +28013-4 0 00001
2 17590 70.9992 131.0227 0004930 350.6797 9.4234 14.17170494 09
| Epoch (UTC): | 17 May 2026 17:22:11 |
| Eccentricity: | 0.0004930 |
| inclination: | 70.9992° |
| perigee height: | 831 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 131.0227° |
| argument of perigee: | 350.6797° |
| revolutions per day: | 14.17170494 |
| mean anomaly at epoch: | 9.4234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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