Long-range constraints on the AdS radius of curvature L in the
Randall-Sundrum (RS) braneworld model are inferred from orbital motions of well
known artificial and natural bodies. Thus, they do not rely upon more or less
speculative and untested theoretical assumptions, contrary to other long-range
RS tests proposed in astrophysical scenarios in which many of the phenomena
adopted may depend on the system's composition, formation and dynamical history
as well. The perihelion precession of Mercury and its radiotechnical ranging
from the Earth yield L <= 10 - 50 km. Tighter bounds come from the perigee
precession of the Moon, from which it can be inferred L <= 500-700 m. The best
constraints (L <= 5 m) come from the Satellite-to-Satellite Tracking (SST)
range of the GRACE A/B spacecrafts orbiting the Earth: proposed follow-on of
such a mission, implying a subnm s-1 range-rate accuracy, may constrain L at
\sim 10 cm level. Weaker constraints come from the double pulsar system (L <=
80 - 100 km) and from the main sequence star S2 orbiting the compact object in
Sgr A* (L <= 6.2 - 8.8 AU). Such bounds on the length L, which must not
necessarily be identified with the AdS radius of curvature of the RS model,
naturally translate into constraints on an, e.g., universal coupling parameter
K of the r^-3 interaction. GRACE yields K <= 1 10^16 m^5 s^-2.Comment: LaTex2e, 6 pages, 2 figures, 2 tables, 64 references. Accepted for
publication in Annalen der Physik. arXiv admin note: substantial text overlap
with arXiv:1112.352