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Traceback (most recent call last):
  File "C:/Users/taiko/PycharmProjects/untitled/solar_system_toy.py", line 125, in <module>
    orbit_list[idx] = orbit_list[idx].propagate(1*u.day,method=cowell,ad=ad)
  File "C:\Users\taiko\AppData\Local\Programs\Python\Python37-32\lib\site-packages\poliastro\twobody\orbit.py", line 999, in propagate
    cartesian = propagate(self, time_of_flight, method=method, rtol=rtol, **kwargs)
  File "C:\Users\taiko\AppData\Local\Programs\Python\Python37-32\lib\site-packages\poliastro\twobody\propagation.py", line 468, in propagate
    orbit.attractor.k, orbit.r, orbit.v, time_of_flight.to(u.s), rtol=rtol, **kwargs
  File "C:\Users\taiko\AppData\Local\Programs\Python\Python37-32\lib\site-packages\poliastro\twobody\propagation.py", line 105, in cowell
    dense_output=True,
  File "C:\Users\taiko\AppData\Local\Programs\Python\Python37-32\lib\site-packages\scipy\integrate\_ivp\ivp.py", line 477, in solve_ivp

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#!/usr/bin/env python3.4

"""
observe_skyfield.py

Observing exercise with Skyfield.
"""

import numpy as np

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#!/usr/bin/env python3
import numpy as np
from skyfield.api import Topos, load
from skyfield.api import EarthSatellite
import matplotlib.pyplot as plt
from matplotlib.patches import Circle
import astropy.units as u
from astropy.wcs import wcs

if __name__ == "__main__":

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#!/usr/bin/env python
"""
Find out where Mars is, in the sky at P'diddy Island, PEI, ON, Canada.
"""

import datetime

# ! pip install skyfield
from skyfield.api import load, Topos

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from skyfield.api import Topos, load
import socket
from time import sleep
import re
import array as arr

#connecting to server 
s = socket.socket(socket.AF_INET, socket.SOCK_STREAM)
s.connect(('where.satellitesabove.me', 5021))
print("connecting to where.satellitesabove.me:5021")

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from tkinter import *
from skyfield.api import Topos, load
import motor

ts = load.timescale()
#Motor al laser
m1 = motor.Motor([18, 22, 24, 26], mode = 3)
m1.rpm = 10
#Motor a la base
m2 = motor.Motor([17,25,12,16], mode = 3)

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# python 3.7 suggested

import datetime
import time
from skyfield.api import load, Topos, EarthSatellite

TLE_FILE = "https://celestrak.com/NORAD/elements/active.txt"
ISS_NAME = "ISS (ZARYA)"
LONGITUDE = -73.9940702
LATITUDE = 40.7546283

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from skyfield.api import load
from jdutil import *

planets = load('de432s.bsp')
earth, jupiter = planets['EARTH'], planets['JUPITER BARYCENTER']
ts = load.timescale()
t = ts.now() 
timenow = jd_to_datetime(float(t.tt))
astrometric = earth.at(t).observe(jupiter)
ra, dec, distance = astrometric.radec()

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#!/usr/bin/env python3

from datetime import datetime, timezone
from math import atan, atan2, degrees, floor, pi, radians, sin, sqrt

from skyfield.api import earth, JulianDate, now, sun


def earth_latlon(x, y, z, time):
    """

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#!/usr/bin/env python3

import sys
from skyfield.api import load, utc
from datetime import datetime


TS_ZERO = datetime(1970, 1, 1)
NAMES = ['朔', '上弦', '望', '下弦']