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4G 5:25 AM P 21:08 James Dior04 Yesterday, 9:40 PM685E2551FC4 О Satellite Earth 1.59 68 K/S 86 Dr. Olakunle Ogunjabi (Department of PhysiPHY 101: Comprehensive Gravitation and Or 2025 Academic Session Assignment: Python Implementation (Group 3) Solve the following problems using Python: Verify Kepler's Third Law for a planet orbiting the Sun: • Semi-major axis: a= (Last 2 digits of your matric number 10) km Mass of Sun: Msun = 1:989 1030 kg Compute the orbital period and compare it with Kepler's equati 296 15/17 4 2³ T²= GM Sun << Simulate the elliptical orbit of a planet around the Sun using Kepler's laws. Plot the trajectory of the planet and indicate the perihelion and aphelion. Submission Deadline: Monday, 17 February 2025. Submit to: Mr. John, Physics Department. Dr. Olakunle Ogunjabi (Department of PhysiPHY 101: Comprehensive Gravitation and Or 2025 Academic Session 560 16/17 Summary Topics Covered: •Newton's Law of Gravitation Kepler's Laws of Planetary Motion Gravitational Potential Energy Escape Velocity • Orbital Mechanics Satellite Applications Next Steps: emnt the assignment using Python Send Share Delete Ո Reply More

4G 5:25 AM P 21:08 James Dior04 Yesterday, 9:40 PM685E2551FC4 О Satellite Earth 1.59 68 K/S 86 Dr. Olakunle Ogunjabi (Department of PhysiPHY 101: Comprehensive Gravitation and Or 2025 Academic Session Assignment: Python Implementation (Group 3) Solve the following problems using Python: Verify Kepler's Third Law for a planet orbiting the Sun: • Semi-major axis: a= (Last 2 digits of your matric number 10) km Mass of Sun: Msun = 1:989 1030 kg Compute the orbital period and compare it with Kepler's equati 296 15/17 4 2³ T²= GM Sun << Simulate the elliptical orbit of a planet around the Sun using Kepler's laws. Plot the trajectory of the planet and indicate the perihelion and aphelion. Submission Deadline: Monday, 17 February 2025. Submit to: Mr. John, Physics Department. Dr. Olakunle Ogunjabi (Department of PhysiPHY 101: Comprehensive Gravitation and Or 2025 Academic Session 560 16/17 Summary Topics Covered: •Newton's Law of Gravitation Kepler's Laws of Planetary Motion Gravitational Potential Energy Escape Velocity • Orbital Mechanics Satellite Applications Next Steps: emnt the assignment using Python Send Share Delete Ո Reply More

Power System Analysis and Design (MindTap Course List)
Power System Analysis and Design (MindTap Course List)
6th Edition
ISBN:9781305632134
Author:J. Duncan Glover, Thomas Overbye, Mulukutla S. Sarma
Publisher:J. Duncan Glover, Thomas Overbye, Mulukutla S. Sarma
Chapter6: Power Flows
Section: Chapter Questions
Problem 6.22P
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4G 5:25 AM P 21:08 James Dior04 Yesterday, 9:40 PM685E2551FC4 О Satellite Earth 1.59 68 K/S 86 Dr. Olakunle Ogunjabi (Department of PhysiPHY 101: Comprehensive Gravitation and Or 2025 Academic Session Assignment: Python Implementation (Group 3) Solve the following problems using Python: Verify Kepler's Third Law for a planet orbiting the Sun: • Semi-major axis: a= (Last 2 digits of your matric number 10) km Mass of Sun: Msun = 1:989 1030 kg Compute the orbital period and compare it with Kepler's equati 296 15/17 4 2³ T²= GM Sun << Simulate the elliptical orbit of a planet around the Sun using Kepler's laws. Plot the trajectory of the planet and indicate the perihelion and aphelion. Submission Deadline: Monday, 17 February 2025. Submit to: Mr. John, Physics Department. Dr. Olakunle Ogunjabi (Department of PhysiPHY 101: Comprehensive Gravitation and Or 2025 Academic Session 560 16/17 Summary Topics Covered: •Newton's Law of Gravitation Kepler's Laws of Planetary Motion Gravitational Potential Energy Escape Velocity • Orbital Mechanics Satellite Applications Next Steps: emnt the assignment using Python Send Share Delete Ո Reply More
Transcribed Image Text:4G 5:25 AM P 21:08 James Dior04 Yesterday, 9:40 PM685E2551FC4 О Satellite Earth 1.59 68 K/S 86 Dr. Olakunle Ogunjabi (Department of PhysiPHY 101: Comprehensive Gravitation and Or 2025 Academic Session Assignment: Python Implementation (Group 3) Solve the following problems using Python: Verify Kepler's Third Law for a planet orbiting the Sun: • Semi-major axis: a= (Last 2 digits of your matric number 10) km Mass of Sun: Msun = 1:989 1030 kg Compute the orbital period and compare it with Kepler's equati 296 15/17 4 2³ T²= GM Sun << Simulate the elliptical orbit of a planet around the Sun using Kepler's laws. Plot the trajectory of the planet and indicate the perihelion and aphelion. Submission Deadline: Monday, 17 February 2025. Submit to: Mr. John, Physics Department. Dr. Olakunle Ogunjabi (Department of PhysiPHY 101: Comprehensive Gravitation and Or 2025 Academic Session 560 16/17 Summary Topics Covered: •Newton's Law of Gravitation Kepler's Laws of Planetary Motion Gravitational Potential Energy Escape Velocity • Orbital Mechanics Satellite Applications Next Steps: emnt the assignment using Python Send Share Delete Ո Reply More
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