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 17567U 26040.29234039 +.00000000 +00000-0 +61409-4 0 00007
2 17567 82.5290 119.4537 0018131 359.7910 0.3296 14.86104999 03
| Epoch (UTC): | 09 February 2026 07:00:58 |
| Eccentricity: | 0.0018131 |
| inclination: | 82.5290° |
| perigee height: | 597 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 119.4537° |
| argument of perigee: | 359.7910° |
| revolutions per day: | 14.86104999 |
| mean anomaly at epoch: | 0.3296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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