Litcius/Paper detail

LARES-2 contribution to global geodetic parameters from the combined LAGEOS-LARES solutions

Krzysztof Sośnica, Filip Gałdyn, Radosław Zajdel, Dariusz Strugarek, Joanna Najder, Adrian Nowak, Marcin Mikoś, Tomasz Kur, Jarosław Bosy, Grzegorz Bury

2024Journal of Geodesy11 citationsDOIOpen Access PDF

Abstract

Abstract LARES-2 is a new geodetic satellite designed for high-accuracy satellite laser ranging. The orbit altitude of LARES-2 is similar to that of LAGEOS-1, whereas the inclination angle of 70° complements the LAGEOS-1 inclination of 110°; hence, both satellites form the butterfly configuration for the verification of the Lense–Thirring effect. Although the major objective of LARES-2 is testing general relativity, LARES-2 substantially contributes to geodesy in terms of the realization of terrestrial reference frames, recovery of the geocenter motion, pole coordinates, length-of-day, and low-degree gravity field coefficients. We analyze the first 1.5 years of LARES-2 data and test different empirical orbit models for LARES-2 with and without co-estimating low-degree gravity field coefficients to find the best combination strategy with LAGEOS satellites. We found that LARES-2 orbit determination is more accurate than that of LAGEOS-1/2 due to a different satellite construction consisting of a solid sphere with no inner structure. Neither the correction for D 0 nor the empirical once-per-revolution along-track accelerations S C / S S have to be estimated for LARES-2 when co-estimating gravity field coefficients. The only empirical parameter needed for LARES-2 is the constant along-track acceleration S 0 to compensate for the Yarkovsky–Schach effect. On the contrary, for LAGEOS-1/2, the non-gravitational perturbations affect C 30 and Z geocenter estimates when once-per-revolution parameters are not estimated. LARES-2 does not face this issue. LARES-2 improves the formal errors of the Z geocenter component by up to 59% and C 20 by up to 40% compared to the combined LAGEOS-1/2 solutions and provides C 30 estimates unaffected by thermal orbit modeling issues.

Topics & Concepts

GeodesyGeodetic datumGravitational fieldOrbit determinationSatelliteGeopotentialSatellite laser rangingOrbit (dynamics)PhysicsDoris (gastropod)RetroreflectorGeologyClassical mechanicsComputer scienceAerospace engineeringAstronomyLaser rangingOpticsLaserEngineeringTelecommunicationsGeophysics and Gravity MeasurementsGNSS positioning and interferenceIonosphere and magnetosphere dynamics