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 17192U 26074.60395161 +.00000000 +00000-0 +43309-4 0 00006
2 17192 82.5064 136.5885 0016353 11.0549 141.7326 14.85919556 08
| Epoch (UTC): | 15 March 2026 14:29:41 |
| Eccentricity: | 0.0016353 |
| inclination: | 82.5064° |
| perigee height: | 599 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 136.5885° |
| argument of perigee: | 11.0549° |
| revolutions per day: | 14.85919556 |
| mean anomaly at epoch: | 141.7326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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