Plotting in 3D

import numpy as np

from poliastro.bodies import Earth, Sun
from poliastro.constants import J2000
from poliastro.examples import churi, iss, molniya
from poliastro.plotting import OrbitPlotter
from poliastro.plotting.orbit.backends import Plotly3D
from poliastro.twobody import Orbit

churi.plot(backend=Plotly3D())

frame = OrbitPlotter(backend=Plotly3D())

frame.plot(churi)
frame.plot_body_orbit(Earth, J2000)
frame.show()

frame = OrbitPlotter(backend=Plotly3D())

frame.plot(molniya)
frame.plot(iss)
frame.show()

eros = Orbit.from_sbdb("eros")

frame = OrbitPlotter(backend=Plotly3D())

frame.plot_body_orbit(Earth, J2000)
frame.plot(eros, label="eros")
frame.show()

from astropy.time import Time
from poliastro.ephem import Ephem
from poliastro.util import time_range

date_launch = Time("2011-11-26 15:02", scale="utc").tdb
date_arrival = Time("2012-08-06 05:17", scale="utc").tdb

earth = Ephem.from_body(
    Earth, time_range(date_launch, end=date_arrival, num_values=50)
)

frame = OrbitPlotter(backend=Plotly3D())
frame.set_attractor(Sun)

frame.plot_body_orbit(Earth, J2000, label=Earth)
frame.plot_ephem(earth, label=Earth)
frame.show()

frame = OrbitPlotter(backend=Plotly3D())

frame.plot(eros, label="eros")
frame.plot_trajectory(earth.sample(), label=str(Earth))
frame.show()