diff --git a/Satellite_Orbits_2nd_Projects.py b/Satellite_Orbits_2nd_Projects.py
new file mode 100644
index 0000000..4fd3c4f
--- /dev/null
+++ b/Satellite_Orbits_2nd_Projects.py
@@ -0,0 +1,68 @@
+
+
+import numpy as np
+import matplotlib.pyplot as plt
+from mpl_toolkits.mplot3d import Axes3D
+
+# Earth parameters
+earth_radius = 6371  # Earth radius in kilometers
+
+# Satellite orbit data
+num_satellites = 10
+inclination_angle = 45  # Orbit inclination angle in degrees
+
+# Generate random semi-major axes and eccentricities for satellite orbits
+semi_major_axes = np.random.uniform(800, 1500, num_satellites)
+eccentricities = np.random.uniform(0.1, 0.4, num_satellites)
+
+# Time array
+num_frames = 100
+time = np.linspace(0, 2 * np.pi, num_frames)
+
+# Set up the figure and axes
+fig = plt.figure()
+ax = fig.add_subplot(111, projection='3d')
+
+# Plotting the Earth
+u = np.linspace(0, 2 * np.pi, 100)
+v = np.linspace(0, np.pi, 50)
+x_earth = earth_radius * np.outer(np.cos(u), np.sin(v))
+y_earth = earth_radius * np.outer(np.sin(u), np.sin(v))
+z_earth = earth_radius * np.outer(np.ones(np.size(u)), np.cos(v))
+ax.plot_surface(x_earth, y_earth, z_earth, color='lightblue')
+
+# Plotting the satellite orbits
+for i in range(num_satellites):
+    semi_major_axis = semi_major_axes[i]
+    eccentricity = eccentricities[i]
+
+    # Parametric equations for satellite orbit
+    r = semi_major_axis * (1 - eccentricity ** 2) / (1 + eccentricity * np.cos(time))
+    x_satellite = r * np.cos(time)
+    y_satellite = r * np.sin(time)
+    z_satellite = np.zeros_like(x_satellite)
+
+    # Rotate orbit inclination
+    angle = np.radians(inclination_angle)
+    x_satellite, y_satellite, z_satellite = (
+        x_satellite * np.cos(angle) - z_satellite * np.sin(angle),
+        y_satellite,
+        x_satellite * np.sin(angle) + z_satellite * np.cos(angle)
+    )
+
+    # Plot satellite orbit
+    ax.plot(x_satellite, y_satellite, z_satellite, color='gray')
+
+# Plotting the invisible red dot satellite
+ax.plot([0], [0], [0], marker='o', markersize=8, color='red', alpha=0.0)
+
+# Set plot labels and limits
+ax.set_xlabel('X (km)')
+ax.set_ylabel('Y (km)')
+ax.set_zlabel('Z (km)')
+ax.set_title('Satellite Orbits')
+
+# Set plot aspect ratio to be equal
+ax.set_box_aspect([1, 1, 1])
+
+plt.show()