Closed-Form Statistical Relations Between Projected Separation, Semimajor Axis, Companion Mass, and Host Acceleration

I derive the statistical relationship between a radial velocity or astrometric acceleration (a trend), a companion’s mass, and the projected separation of the companion. These relationships, expressed as probability density functions, are analytic and independent of all Keplerian orbital elements so long as orbits are randomly oriented in space. I also derive a closed-form expression for the probability distribution of the ratio of the projected separation to the semimajor axis at fixed eccentricity. This expression can be numerically integrated over eccentricity for an arbitrary distribution of eccentricities. I verify my results with empirical comparisons to equivalent but more complex expressions in the literature based on the equations of Keplerian orbits. The closed-formed expressions derived here would be especially useful for any calculation that requires derivatives, e.g., Hamiltonian Monte Carlo. I also provide a Jupyter notebook including all figures and calculations (at https://github.com/t-brandt/analytic-orbit-calculations).

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Publication Details

Journal
The Open Journal of Astrophysics
Published
2026-04-17
DOI
https://doi.org/10.33232/001c.160757
Primary Topic
Spacecraft Dynamics and Control
Type
article
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article

Closed-Form Statistical Relations Between Projected Separation, Semimajor Axis, Companion Mass, and Host Acceleration

Timothy D. Brandt
The Open Journal of Astrophysics
Spacecraft Dynamics and Control
article

Closed-Form Statistical Relations Between Projected Separation, Semimajor Axis, Companion Mass, and Host Acceleration

Timothy D. Brandt
article en

Abstract

I derive the statistical relationship between a radial velocity or astrometric acceleration (a trend), a companion’s mass, and the projected separation of the companion. These relationships, expressed as probability density functions, are analytic and independent of all Keplerian orbital elements so long as orbits are randomly oriented in space. I also derive a closed-form expression for the probability distribution of the ratio of the projected separation to the semimajor axis at fixed eccentricity. This expression can be numerically integrated over eccentricity for an arbitrary distribution of eccentricities. I verify my results with empirical comparisons to equivalent but more complex expressions in the literature based on the equations of Keplerian orbits. The closed-formed expressions derived here would be especially useful for any calculation that requires derivatives, e.g., Hamiltonian Monte Carlo. I also provide a Jupyter notebook including all figures and calculations (at https://github.com/t-brandt/analytic-orbit-calculations).

The Open Journal of AstrophysicsVol. 9
ORCID (US)
Openalex Percentile: Top 6%
Spacecraft Dynamics and Control
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