Ch3_Space_Flight_Dyna... SPST305-W3-Key Equation... SPST 305 W4HW Assig... X SPST305_W4HW.docx.pdf SPST305_W4HW_TefftK.docx... Space_Flight_Dynamics_... + Create All tools Edit Convert E-Sign Find text or tools Q | All tools 1 An update is available for generative Al features (beta) in Acrobat. Please relaunch Acrobat to enable it. Restart Acrobat Learn More Export a PDF Edit a PDF SPST 305 Week 4 Homework Assignment Request e-signatures In preparation for this Homework Assignment, review the information in this Week's Lesson Readings Fill & Sign and Read Chapter 4 of our Textbook, then Respond the Following Questions (Assume the average e Earth Radius RE = 6378 km) Create a PDF [A] Answer questions 1 - 7 based on the following information: A reconnaissance satellite has an apogee Stylize this PDF NEW altitude of alta = 6822 km and a perigee altitude of alt = 1542 km. The current true anomaly is Oinitial = 1960. Use 3 decimal places (or 3 significant figures for