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عناصر مداری · Vinony

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عناصر مداری

🌐فارسی

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EntityQ272626· pop 46· linked from 613 articles

عناصر مداری

parameters required to uniquely identify a specific orbit

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orbital inclination

Entity

orbital eccentricity

two-body problem

North American Aerospace Defense Command

Kozai mechanism

longitude of the periapsis

near-equatorial orbit

Carl Friedrich Gauss

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Similar entities

Discovered by embedding cosine similarity (sentence-transformers MiniLM, 384-dim).

Entitydist 0.44

co-orbital configuration

Entitydist 0.46

Entitydist 0.47

Entitydist 0.53

Entitydist 0.53

Entitydist 0.53

Entitydist 0.54

Entitydist 0.54

Entitydist 0.54

Entitydist 0.55

Entitydist 0.55

planetary system

Entitydist 0.56

What links here613 pages

geocentric orbit

argument of periapsis

orbital inclination

eccentric anomaly

orbit determination

Orbital state vectors

asteroid family

orbital station-keeping

interplanetary transport network