diff --git a/docs/static/pr_examples/cp_evolution_calisto_like.png b/docs/static/pr_examples/cp_evolution_calisto_like.png
new file mode 100644
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diff --git a/docs/static/pr_examples/cp_evolution_to_apogee.png b/docs/static/pr_examples/cp_evolution_to_apogee.png
new file mode 100644
index 000000000..5d0036ee6
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diff --git a/rocketpy/plots/flight_plots.py b/rocketpy/plots/flight_plots.py
index 6dd5e8802..d9d63e168 100644
--- a/rocketpy/plots/flight_plots.py
+++ b/rocketpy/plots/flight_plots.py
@@ -2897,6 +2897,92 @@ def fluid_mechanics_data(self, *, filename=None):  # pylint: disable=too-many-st
         plt.subplots_adjust(hspace=0.5)
         show_or_save_plot(filename)
 
+    def center_of_pressure(self, *, filename=None):
+        """Plot center-of-pressure position evolution through flight time.
+
+        The rocket center of pressure is a function of Mach number. This method
+        evaluates it at the flight Mach number at each time step and plots the
+        resulting position against time. Center of mass is shown on the same
+        axis for context, and static margin is shown on a twin axis.
+
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved. Supported file endings are:
+            eps, jpg, jpeg, pdf, pgf, png, ps, raw, rgba, svg, svgz, tif, tiff
+            and webp (these are the formats supported by matplotlib).
+
+        Returns
+        -------
+        None
+        """
+        time = self.flight.mach_number[:, 0]
+        mask = time <= self.first_event_time
+        time = time[mask]
+        mach = self.flight.mach_number[:, 1][mask]
+
+        center_of_pressure = self.flight.rocket.cp_position.get_value_opt(mach)
+        center_of_mass = self.flight.rocket.center_of_mass.get_value_opt(time)
+        static_margin = self.flight.rocket.static_margin.get_value_opt(time)
+
+        plt.figure(figsize=(9, 6))
+        ax1 = plt.subplot(111)
+        (line_cp,) = ax1.plot(
+            time,
+            center_of_pressure,
+            color="#1f77b4",
+            label="Center of Pressure",
+        )
+        (line_cm,) = ax1.plot(
+            time,
+            center_of_mass,
+            color="#ff7f0e",
+            label="Center of Mass",
+        )
+        ax1.set_xlim(0, self.first_event_time)
+        ax1.set_title("Center of Pressure Evolution")
+        ax1.set_xlabel("Time (s)")
+        ax1.set_ylabel("Position (m)")
+        ax1.grid(True)
+
+        ax2 = ax1.twinx()
+        (line_sm,) = ax2.plot(
+            time,
+            static_margin,
+            color="#2ca02c",
+            linestyle="--",
+            label="Static Margin",
+        )
+        ax2.set_ylabel("Static Margin (c)", color="#2ca02c")
+        ax2.tick_params("y", colors="#2ca02c")
+
+        event_lines = [
+            ax1.axvline(
+                x=self.flight.out_of_rail_time,
+                color="r",
+                linestyle="--",
+                label="Out of Rail Time",
+            ),
+            ax1.axvline(
+                x=self.flight.rocket.motor.burn_out_time,
+                color="g",
+                linestyle=":",
+                label="Burn Out Time",
+            ),
+            ax1.axvline(
+                x=self.flight.apogee_time,
+                color="m",
+                linestyle="--",
+                label="Apogee Time",
+            ),
+        ]
+
+        lines = [line_cp, line_cm, line_sm, *event_lines]
+        ax1.legend(lines, [line.get_label() for line in lines], loc="best")
+
+        show_or_save_plot(filename)
+
     def stability_and_control_data(self, *, filename=None):  # pylint: disable=too-many-statements
         """Prints out Rocket Stability and Control parameters graphs available
         about the Flight
@@ -3101,6 +3187,9 @@ def all(self):  # pylint: disable=too-many-statements
         print("\n\nTrajectory Stability and Control Plots\n")
         self.stability_and_control_data()
 
+        print("\n\nCenter of Pressure Evolution Plot\n")
+        self.center_of_pressure()
+
         print("\n\nRocket and Parachute Pressure Plots\n")
         self.pressure_rocket_altitude()
         self.pressure_signals()
diff --git a/tests/unit/test_plots.py b/tests/unit/test_plots.py
index 7f21dcdd7..d6a529e8b 100644
--- a/tests/unit/test_plots.py
+++ b/tests/unit/test_plots.py
@@ -448,6 +448,29 @@ def test_animation_options_validation_errors(kwargs, error):
         _FlightPlots._animation_options(kwargs)
 
 
+@patch("matplotlib.pyplot.show")
+@pytest.mark.parametrize("filename", [None, "test_cp_evolution.png"])
+def test_flight_center_of_pressure_plot(mock_show, filename, flight_calisto):  # pylint: disable=unused-argument
+    """Center-of-pressure evolution plot runs for a fixture flight.
+
+    Parameters
+    ----------
+    mock_show :
+        Mocks the matplotlib.pyplot.show() function to avoid showing the plots.
+    filename : str | None
+        Destination path, or None to show the plot.
+    flight_calisto : rocketpy.Flight
+        Flight object to be used in the tests. See conftest.py for more details.
+    """
+    assert flight_calisto.plots.center_of_pressure(filename=filename) is None
+    if filename is None:
+        mock_show.assert_called_once()
+    else:
+        assert os.path.exists(filename)
+        os.remove(filename)
+    plt.close("all")
+
+
 def test_ground_bounds_from_spec(flight_calisto):
     """Ground image bounds convert from ENU and lat/lon, and validate input."""
     plots = flight_calisto.plots