Increase Data Rate?

[PowerBroker2]

I'm trying to get real-time location and attitude data, but it seems I can only get a ~5Hz data rate using this lib. I'd prefer to stay in Python and not switch to the C++ SDK, so I figure I'd ask here: Is there a way to speed up the data rate?

Here is my current code for reference:

import sys
from os.path import dirname
from pprint import pprint

import numpy as np
from SimConnect import *

SIM_DIR = dirname(__file__)
SRC_DIR = dirname(SIM_DIR)
sys.path.append(SIM_DIR)
sys.path.append(SRC_DIR)

import rotation
import pilotUtils


sm = SimConnect()
aq = AircraftRequests(sm, _time=0)

while not sm.quit:
    lat = aq.PositionandSpeedData.get('PLANE_LATITUDE')
    lon = aq.PositionandSpeedData.get('PLANE_LONGITUDE')
    alt = aq.PositionandSpeedData.get('PLANE_ALTITUDE') 
    
    alt_agl = aq.PositionandSpeedData.get('PLANE_ALT_ABOVE_GROUND')
    
    roll  = aq.PositionandSpeedData.get('PLANE_BANK_DEGREES')
    pitch = aq.PositionandSpeedData.get('PLANE_PITCH_DEGREES')
    yaw   = aq.PositionandSpeedData.get('PLANE_HEADING_DEGREES_TRUE')
    
    airspeed = aq.FlightInstrumentationData.get('AIRSPEED_TRUE')
    
    if None not in [lat, lon, alt, alt_agl, roll, pitch, yaw, airspeed]:
        lla = np.array([lat,           # dd
                        lon,           # dd
                        alt / 3.2808]) # Ft -> m above MSL

        agl = alt_agl / 3.2808 # Ft -> m above AGL

        B_angles_N = np.rad2deg(np.array([-roll,  # Actually radians
                                          -pitch, # Actually radians
                                          yaw]))  # Actually radians
        B_dcm_N = rotation.angle2dcm(B_angles_N,
                                     pilotUtils.DEGREES,
                                     True,
                                     321).squeeze()

        B_airspeed = np.array([airspeed * 0.514444, # Knots -> m/s
                               0,
                               0])
        N_airspeed = B_dcm_N.T @ B_airspeed
        
        pprint(lla)
        pprint(B_angles_N)
        pprint(B_airspeed)
        pprint(N_airspeed)
        print('')