Improvement of orbit precision by addition of radio data: example of the fireball of October 15, 2018.
|Sensor||Initial velocity||Effective surface / mass ratio|
|km s−1||m2 kg−1|
|Video||66.49 ± 0.92||<1.28|
|Radio+Video||66.09 ± 0.09||0.33 ± 0.14|
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