Classifier Instance:

Anchor text: LEO
Target Entity: Low_Earth_orbit
Preceding Context: Suppose we want to send a 10,000 kg space probe to Mars. The required \Delta v from
Succeeding Context: is approximately 3000 m/s, using a Hohmann transfer orbit. For the sake of argument, let us say that the following thrusters may be used:
Paragraph Title: Example
Source Page: Spacecraft propulsion

Ground Truth Types:

|---wordnet_entity_100001740
|  |---yagoGeoEntity
|  |  |---wordnet_location_100027167
|  |  |  |---wordnet_line_108593262
|  |  |  |  |---wordnet_path_108616311

Predicted Types:

TypeConfidenceDecision
wordnet_artifact_100021939-0.5349499031721113 0
wordnet_event_100029378-1.4059449102086687 0
wordnet_organization_108008335-1.562533024118226 0
wordnet_person_100007846-0.23868454572218337 0
yagoGeoEntity-0.3132583223365777 0
|---wordnet_entity_100001740
|  |---wordnet_artifact_100021939
|  |---wordnet_event_100029378
|  |---wordnet_organization_108008335
|  |---wordnet_person_100007846
|  |---yagoGeoEntity