How to use the poliastro.plotting.static.StaticOrbitPlotter function in poliastro

def test_set_frame_plots_same_colors():
    # TODO: Review
    op = StaticOrbitPlotter()
    op.plot_body_orbit(Jupiter, J2000)
    colors1 = [orb[2] for orb in op.trajectories]
    op.set_body_frame(Jupiter)
    colors2 = [orb[2] for orb in op.trajectories]
    assert colors1 == colors2

def test_plot_trajectory_sets_label():
    expected_label = "67P"

    op = StaticOrbitPlotter()
    trajectory = churi.sample()
    op.plot_body_orbit(Mars, J2000, label="Mars")

    op.plot_trajectory(trajectory, label=expected_label)

    legend = plt.gca().get_legend()
    assert legend.get_texts()[1].get_text() == expected_label

def test_basic_trajectory_plotting():
    fig, ax = plt.subplots()
    plotter = StaticOrbitPlotter(ax=ax)
    plotter.set_attractor(Earth)
    plotter.set_orbit_frame(iss)
    plotter.plot_trajectory(iss.sample())

    return fig

def test_plot_ephem_no_epoch():
    epoch = Time("2020-02-14 00:00:00")
    ephem = Ephem.from_horizons(
        "2020 CD3",
        time_range(Time("2020-02-13 12:00:00"), end=Time("2020-02-14 12:00:00")),
        attractor=Earth,
    )

    fig, ax = plt.subplots()
    plotter = StaticOrbitPlotter(ax=ax)
    plotter.set_attractor(Earth)
    plotter.set_orbit_frame(Orbit.from_ephem(Earth, ephem, epoch))

    plotter.plot_ephem(ephem, label="2020 CD3 Minimoon", color="k")

    return fig

def test_color():
    op = StaticOrbitPlotter()
    ss = iss
    c = "#FF0000"
    op.plot(ss, label="ISS", color=c)
    ax = plt.gca()

    assert ax.get_legend().get_lines()[0].get_c() == c
    for element in ax.get_lines():
        assert element.get_c() == c

def test_redraw_makes_attractor_none():
    # TODO: Review
    op = StaticOrbitPlotter()
    op._redraw()
    assert op._attractor_radius is not None

def test_dark_mode_plots_dark_plot(dark, expected_color):
    op = StaticOrbitPlotter(dark=dark)
    assert op._ax.get_facecolor() == expected_color

def test_basic_orbit_and_trajectory_plotting():
    fig, ax = plt.subplots()
    plotter = StaticOrbitPlotter(ax=ax)
    plotter.plot(iss)
    plotter.plot_trajectory(molniya.sample(), label="Molniya")

    return fig

def test_trail_plotting():
    fig, ax = plt.subplots()
    plotter = StaticOrbitPlotter(ax=ax)
    plotter.plot(iss, trail=True)

    return fig

def test_legend():
    op = StaticOrbitPlotter()
    ss = iss
    op.plot(ss, label="ISS")
    legend = plt.gca().get_legend()

    ss.epoch.out_subfmt = "date_hm"
    label = f"{ss.epoch.iso} (ISS)"

    assert legend.get_texts()[0].get_text() == label