ᴇsᴛɪᴍᴀᴛɪᴏɴ ᴏғ sᴀᴛᴇʟʟɪᴛᴇ ᴏʀʙɪᴛᴀʟ ᴇʟᴇᴍᴇɴᴛ - ɪs ᴛʀᴜᴇ ʟᴏɴɢɪᴛᴜᴅᴇ / ᴍᴇᴀɴ ʟᴏɴɢɪᴛᴜᴅᴇ / ᴀʀɢᴜᴍᴇɴᴛ ᴏғ ʟᴀᴛɪᴛᴜᴅᴇ ʟɪɴᴇᴀʀ?
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Argument of Perigee, ω. This angle describes the orientation of an orbit within its orbital plane. It is the angle between the ascending node and perigee, measured in the direction of the spacecraft's motion. Figure 4.1.
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