Astronomy
ESA PB05-Style Brouwer–Lyddane Averaged-Element Orbit Propagator (J2–J6 + Luni-solar)
Propagate near-Earth and GNSS-region orbits with a semi-analytical averaged-element model in the Brouwer–Lyddane / PB05 tradition: orbit-averaged secular drift of the mean elements under the EGM96 zonal field J2–J6 (numerical Gauss-equation averaging — the Delaunay-normalisation analogue with the closed-form J2 rates as a built-in cross-check), first-order J2 short-period mean↔osculating reconstruction, long-period J3 frozen-orbit analysis (e = −J3·sin i/(2·J2·p), ω = 90°), double-averaged luni-solar quadrupole secular effects on an elliptical inclined perturber orbit (the Celletti/Kozai–Lidov term with the 39.23° critical mutual inclination), tesseral ground-track resonance checks (1:1, 2:1, 3:2, 5:2 and small-rational commensurabilities with Earth rotation), sun-synchronous inclination solving, and an in-report RK4 numerical-propagation cross-validation of the averaged model.
Quick start
Call this tool from your code in three languages.
curl -X POST 'https://api.elysiatools.com/en/api/tools/esa-pb05-pce-pck-reddy-porter-keplerian-equation-averaged-element-propagator' \
-H 'Content-Type: application/json' \
-d '{"semiMajorAxisKm":8000,"eccentricity":0.05,"inclinationDeg":52.5,"raanDeg":30,"argPerigeeDeg":70,"meanAnomalyDeg":0,"durationDays":30,"zonalDepth":"j2-j4","lunisolar":"none","showReconstruction":true}'