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Home/Astronomy & The Sky/Exoplanet Radial Velocity

Exoplanet Radial Velocity

In the two-body problem the star and planet orbit their barycenter. For a circular orbit the star’s line-of-sight velocity is sinusoidal with semi-amplitude K = (M_p/M_tot) √(G M_tot/a) sin i, with a fixed by Kepler’s third law from M_tot and P. Spectroscopy measures Doppler shifts; without knowing inclination i, radial-velocity surveys constrain M_p sin i rather than M_p alone. Stellar activity (“jitter”) and multiple planets add complexity beyond this single-planet, zero-eccentricity model.

Who it's for: Pairs with the transit simulator and spectral Doppler page.

Key terms

  • radial velocity
  • Doppler wobble
  • semi-amplitude
  • M sin i
  • Kepler’s third law

Live graphs

Doppler wobble (circular)

1 M☉
1 M⊕
365 d
1

**K** = (M_p/M_tot) **v_orb** **sin i** with **v_orb** = √(GM_tot/a) and **a** from Kepler’s third law. **Edge-on** (**i** ≈ 90°) gives **sin i** ≈ 1. RV surveys constrain **M_p sin i** when **i** is unknown.

Shortcuts

  • •Lower sin i shrinks the observed wobble (unknown inclination leaves M sin i)

Measured values

K (semi-amplitude)0.089 m/s
M_p (Jupiter units)0.003 M_J
M_p sin i (Earth)1.00 M⊕

How it works

A planet and star orbit their common center of mass. The star’s line-of-sight speed varies with the orbital phase; for a circular orbit the radial velocity is sinusoidal with semi-amplitude K. Larger planet mass, shorter period (smaller a), and higher sin i increase K. Spectrographs measure Doppler shifts of stellar lines; the minimum planet mass is M sin i when inclination is unknown. This page neglects eccentricity and stellar jitter.

Key equations

a³ = G M_tot P² / (4π²) · K = (M_p/M_tot) √(G M_tot/a) sin i
V_r(t) = K sin(2πt/P + φ)

Frequently asked questions

Why M sin i?
The radial component of the wobble scales with sin i for circular orbits. Face-on systems (i near 0) show almost no line-of-sight motion; only edge-on geometries let sin i ≈ 1.
Is eccentricity included?
No — this page uses e = 0. Eccentric orbits add harmonic content and change the effective K.