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# Plotting in 3D

```{code-cell} ipython3
import numpy as np

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

```{code-cell} ipython3
churi.plot(backend=Plotly3D())
```

```{code-cell} ipython3
frame = OrbitPlotter(backend=Plotly3D())

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

```{code-cell} ipython3
frame = OrbitPlotter(backend=Plotly3D())

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

```{code-cell} ipython3
eros = Orbit.from_sbdb("eros")

frame = OrbitPlotter(backend=Plotly3D())

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

```{code-cell} ipython3
from astropy.time import Time
from boinor.ephem import Ephem
from boinor.util import time_range
```

```{code-cell} ipython3
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)
)
```

```{code-cell} ipython3
frame = OrbitPlotter(backend=Plotly3D())
frame.set_attractor(Sun)

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

```{code-cell} ipython3
frame = OrbitPlotter(backend=Plotly3D())

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