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1. Radiated particle detection cloud ch... Radiated particle detection cloud chamber

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   import cv2 as cv

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   import imutils

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   import PIL

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   from PIL import Image, ImageEnhance

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   from scipy.spatial import distance as dist

2. Getting ground station coverage Getting ground station coverage

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   # Load ground stations from CSV

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   import pandas as pd

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   import matplotlib.pyplot as plt

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   import geopandas as gpd

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3. Deorbiting a satellite Deorbiting a satellite

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   % Define input parameters

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   Re = 6378.137;         % Earth Radius (km)

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   initial_altitude = 600; % Initial Altitude (km)

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   a = Re + initial_altitude; % Semi-Major Axis (km)

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   e = 0.001;             % Eccentricity

4. Sun-synchronous orbit for 1U satelli... Sun-synchronous orbit for 1U satellite at 600km

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   % URSA-1 Sun-Synchronous Orbit Simulation

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   % Altitude: 600 km

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   % Inclination: ~97.8° (calculated for sun-synchronous condition)

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   % Eccentricity: 0.001

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   % RAAN: Calculated based on Berlin's location