Triple
T12953698
| Position | Surface form | Disambiguated ID | Type / Status |
|---|---|---|---|
| Subject | EQUULEUS |
E309956
|
entity |
| Predicate | fullName |
P16
|
FINISHED |
| Object |
EQUilibriUm Lunar-Earth point 6U Spacecraft
EQUilibriUm Lunar-Earth point 6U Spacecraft (EQUULEUS) is a JAXA-developed 6U CubeSat designed to demonstrate low-energy trajectory technologies and observe Earth's plasmasphere while operating near the Earth–Moon Lagrange points.
|
E1010247
|
NE FINISHED |
How this triple was built (4 steps)
Every LLM step that produced this triple, in pipeline order — named-entity classification, the disambiguation choices (the exact options shown, with the pick highlighted), and the generated description. The batch + timestamp of each is in the Provenance table below.
NER
Named-entity recognition
gpt-5-mini
Instruction
Given a phrase, classify it is english named entity (e.g., persons, organizations, works of art) in Latin script, or not (e.g., literals, dates, URLs, verbose phrases). For disambiguation, the statement where the phrase occurs as object is also given. Please return a JSON object with `phrase` (string, the phrase being analyzed) and `is_ne` (boolean, indicating whether the phrase is a Named Entity).
Input
Phrase: EQUilibriUm Lunar-Earth point 6U Spacecraft | Statement: [EQUULEUS, fullName, EQUilibriUm Lunar-Earth point 6U Spacecraft]
NED1
Entity disambiguation (via context triple)
gpt-5-mini-2025-08-07
Target entity: EQUilibriUm Lunar-Earth point 6U Spacecraft Context triple: [EQUULEUS, fullName, EQUilibriUm Lunar-Earth point 6U Spacecraft]
-
A.
Earth–Moon L1 point
The Earth–Moon L1 point is a gravitational equilibrium location between Earth and the Moon where spacecraft can maintain a relatively stable position with minimal fuel, often using Lissajous or halo orbits for observation or transfer missions.
-
B.
Lissajous orbit
A Lissajous orbit is a stable, looping three-dimensional trajectory around a Lagrange point, commonly used by space observatories to maintain a relatively constant position with respect to Earth and the Sun.
-
C.
Earth–Moon L2 point
The Earth–Moon L2 point is a gravitationally stable location beyond the Moon where the combined gravity of Earth and the Moon allows spacecraft to maintain a relatively fixed position with minimal fuel.
-
D.
Earth–Moon barycenter
The Earth–Moon barycenter is the common center of mass around which both Earth and the Moon orbit in their mutual gravitational interaction.
-
E.
Sun–Earth L2
Sun–Earth L2 is a gravitationally stable point in space located beyond Earth's orbit where the combined gravity of the Sun and Earth allows spacecraft, such as the James Webb Space Telescope, to maintain a relatively constant position with minimal fuel use.
- F. None of above. chosen
- G. Unsure - the case is ambiguous/there is not enough information to decide.
NEDg
Description generation
gpt-5.1
Instruction
Generate a one-sentence description of the target entity. You are given a context triple in the form (subject, predicate, object), where the object is the target entity. # Instructions Use the triple to infer relevant information about the entity. Describe the entity based on what is most defining, well-known. Avoid repeating the information from the triple, unless really essential. # Response Format Return only the sentence: "Description: [one-sentence description of the target entity]"
Input
Entity: EQUilibriUm Lunar-Earth point 6U Spacecraft Triple: [EQUULEUS, fullName, EQUilibriUm Lunar-Earth point 6U Spacecraft]
Generated description
EQUilibriUm Lunar-Earth point 6U Spacecraft (EQUULEUS) is a JAXA-developed 6U CubeSat designed to demonstrate low-energy trajectory technologies and observe Earth's plasmasphere while operating near the Earth–Moon Lagrange points.
NED2
Entity disambiguation (via description)
gpt-5-mini-2025-08-07
Target entity: EQUilibriUm Lunar-Earth point 6U Spacecraft Target entity description: EQUilibriUm Lunar-Earth point 6U Spacecraft (EQUULEUS) is a JAXA-developed 6U CubeSat designed to demonstrate low-energy trajectory technologies and observe Earth's plasmasphere while operating near the Earth–Moon Lagrange points.
-
A.
Earth–Moon L1 point
The Earth–Moon L1 point is a gravitational equilibrium location between Earth and the Moon where spacecraft can maintain a relatively stable position with minimal fuel, often using Lissajous or halo orbits for observation or transfer missions.
-
B.
Lissajous orbit
A Lissajous orbit is a stable, looping three-dimensional trajectory around a Lagrange point, commonly used by space observatories to maintain a relatively constant position with respect to Earth and the Sun.
-
C.
Earth–Moon L2 point
The Earth–Moon L2 point is a gravitationally stable location beyond the Moon where the combined gravity of Earth and the Moon allows spacecraft to maintain a relatively fixed position with minimal fuel.
-
D.
Earth–Moon barycenter
The Earth–Moon barycenter is the common center of mass around which both Earth and the Moon orbit in their mutual gravitational interaction.
-
E.
Sun–Earth L2
Sun–Earth L2 is a gravitationally stable point in space located beyond Earth's orbit where the combined gravity of the Sun and Earth allows spacecraft, such as the James Webb Space Telescope, to maintain a relatively constant position with minimal fuel use.
- F. None of above. chosen
Provenance (5 batches)
The batch behind each pipeline step, in order, with when it ran. Timestamps are batch-level — stages were processed in waves, so the object chain (NER → NED1 → NEDg → NED2) reads in order, but predicate / elicitation batches can sit in a different wave.
| Step | Stage | Batch ID | Status | When |
|---|---|---|---|---|
| creating | Elicitation | batch_69d7bdfb57a88190836b743e2825feca |
completed | April 9, 2026, 2:55 p.m. |
| NER | Named-entity recognition | batch_69d97e1edcdc8190a702c2a5ea58cc67 |
completed | April 10, 2026, 10:47 p.m. |
| NED1 | Entity disambiguation (via context triple) | batch_69f6af7a10f48190b7e0d32725f83fb6 |
completed | May 3, 2026, 2:14 a.m. |
| NEDg | Description generation | batch_69f6b02f194c8190921aee4cb016a6e2 |
completed | May 3, 2026, 2:17 a.m. |
| NED2 | Entity disambiguation (via description) | batch_69f6b0928ef48190ab4240abbccec5f2 |
completed | May 3, 2026, 2:18 a.m. |
Created at: April 9, 2026, 5:44 p.m.