diff --git a/continue.md b/continue.md
index baf6c1a..a31cd49 100644
--- a/continue.md
+++ b/continue.md
@@ -116,21 +116,21 @@ All constants defined in `src/test_utilities.h` — use those, do not redefine l
 ## Test Refactoring Status
 
 ### Completed
-- `test_barkers_equation` ✅ — Barker's equation unit tests + parabolic propagation
-- `test_cartesian_to_elements_advanced` ✅ — Advanced conversion tests (eccentricity spectrum, inclination, true anomaly, 3D orientation)
-- `test_cartesian_to_elements_basic` ✅ — Element round-trip conversion (semi-major axis, eccentricity, true anomaly, inclination, radius, velocity)
-- `test_parabolic_orbit` ✅ — Parabolic orbit energy conservation + escape trajectory + initial conditions
-- `test_extreme_eccentricity` ✅ — High-eccentricity orbits (single SCENARIO, precalculated values, REL_TOL)
-- `test_extreme_orientation_mixed` ✅ — Extreme orientation conversions, rotation matrix properties, singularity handling
-- `test_extreme_timescales` ✅ — 9 TEST_CASEs → 1 SCENARIO with 11 SECTIONs, all WithinAbs use named constants
-- `test_analytical_propagation` ✅ — 5 SCENARIOs → 1 SCENARIO with 23 SECTIONs, precalculated values, all WithinAbs use named constants
-- `test_moon_orbits` ✅ — Multi-body hierarchical propagation with local/global coordinate tracking
-- `test_energy` ✅ — Energy calculations and conservation tests
-- `test_inclined_orbits` ✅ — 3D inclined orbit conversions, Molniya orbits, rotation matrices
-- `test_maneuvers` ✅ — Impulsive burn tests with precalculated values
-- `test_orbital_period` ✅ — Orbital period calculations, SCENARIO/SECTION pattern
-- `test_true_anomaly_roundtrip` ✅ — True anomaly conversion round-trips, tight tolerances
-- `test_physics_utilities` ✅ — Vector math, acceleration, matrix ops, rotation matrices, compare_vec3
+- `test_barkers_equation` — Barker's equation unit tests + parabolic propagation
+- `test_cartesian_to_elements_advanced` — Advanced conversion tests (eccentricity spectrum, inclination, true anomaly, 3D orientation)
+- `test_cartesian_to_elements_basic` — Element round-trip conversion (semi-major axis, eccentricity, true anomaly, inclination, radius, velocity)
+- `test_parabolic_orbit` — Parabolic orbit energy conservation + escape trajectory + initial conditions
+- `test_extreme_eccentricity` — High-eccentricity orbits (single SCENARIO, precalculated values, REL_TOL)
+- `test_extreme_orientation_mixed` — Extreme orientation conversions, rotation matrix properties, singularity handling
+- `test_extreme_timescales` — 9 TEST_CASEs → 1 SCENARIO with 11 SECTIONs, all WithinAbs use named constants
+- `test_analytical_propagation` — 5 SCENARIOs → 1 SCENARIO with 23 SECTIONs, precalculated values, all WithinAbs use named constants
+- `test_moon_orbits` — Multi-body hierarchical propagation with local/global coordinate tracking
+- `test_energy` — Energy calculations and conservation tests
+- `test_inclined_orbits` — 3D inclined orbit conversions, Molniya orbits, rotation matrices
+- `test_maneuvers` — Impulsive burn tests with precalculated values
+- `test_orbital_period` — Orbital period calculations, SCENARIO/SECTION pattern
+- `test_true_anomaly_roundtrip` — True anomaly conversion round-trips, tight tolerances
+- `test_physics_utilities` — Vector math, acceleration, matrix ops, rotation matrices, compare_vec3
 - `test_periapsis_burn` — prograde burns
 
 ### Can Refactor Now (sim_engine.py supports all features needed)