Precession of Mercury’s Perihelion from Ranging to the MESSENGER Spacecraft
- Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109 (United States)
The perihelion of Mercury’s orbit precesses due to perturbations from other solar system bodies, solar quadrupole moment (J {sub 2}), and relativistic gravitational effects that are proportional to linear combinations of the parametrized post-Newtonian parameters β and γ. The orbits and masses of the solar system bodies are quite well known, and thus the uncertainty in recovering the precession rate of Mercury’s perihelion is dominated by the uncertainties in the parameters J {sub 2}, β, and γ. Separating the effects due to these parameters is challenging since the secular precession rate has a linear dependence on each parameter. Here we use an analysis of radiometric range measurements to the MESSENGER (MErcury Surface, Space ENvironment, GEochemistry, and Ranging) spacecraft in orbit about Mercury to estimate the precession of Mercury’s perihelion. We show that the MESSENGER ranging data allow us to measure not only the secular precession rate of Mercury’s perihelion with substantially improved accuracy, but also the periodic perturbation in the argument of perihelion sensitive to β and γ. When combined with the γ estimate from a Shapiro delay experiment from the Cassini mission, we can decouple the effects due to β and J {sub 2} and estimate both parameters, yielding (β−1)=(−2.7±3.9)×10{sup −5} and J {sub 2} = (2.25 ± 0.09) × 10{sup −7}. We also estimate the total precession rate of Mercury’s perihelion as 575.3100 ± 0.0015″/century and provide estimated contributions and uncertainties due to various perturbing effects.
- OSTI ID:
- 22863119
- Journal Information:
- The Astronomical Journal (Online), Journal Name: The Astronomical Journal (Online) Journal Issue: 3 Vol. 153; ISSN 1538-3881
- Country of Publication:
- United States
- Language:
- English
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