2012年6月1日 · In seconds, our orbital period is: 2,049.351406 EXACTLY. To find this in minutes, simply divide by sixty. At the altitude I mentioned above, it will take exactly 34.15585677 …

2021年7月4日 · The first is the calculation of orbital period from the semi-major axis, and the second is calculation of the semi-major axis from the orbital period. 3 hours ago, …

2014年1月14日 · Ok, I've managed to calculate the orbital period from altitude (first equation), which I tested using the data for a geosynchronous orbit (2868.75km), and I've understood …

2013年6月15日 · The formula for orbital period is as follows: Pi*2 (squareroot) (A^3/U) Where: Pi = 3.14. A = Semi Major Axis of the orbit. U = Gravitational Parameter of parent body. So …

2013年8月2日 · The orbital period is given by 2À√(a³/μ) Where a is the semi major axis (for a circular orbit this is the altitude of the orbit plus the radius of the body) and …

2015年7月13日 · For this, we'll use Kepler's third law, which can be formulated as: "All orbits with the same semi-major axis have the same orbital period." This allows us to calculate the orbital …

2015年4月19日 · Enter your target values. The S button on the same row of the orbital period will set the orbital period to the parent body's rotation period (useful for synchronous orbits). Click …

2021年7月27日 · Enter your target values. The S button on the same row of the orbital period will set the orbital period to the parent body's rotation period (useful for synchronous orbits). Click …

2014年9月19日 · Hy. ATM i started to add some satellites on kerbin orbit ( second attempt , first one ended up with a big de-sync only after 3 day's) . I want to keep them sync. with each other …

2014年4月14日 · For a given central body and a small orbiter, the orbital period only depends on the semi-major axis and none of the other parameters you mention. So just take a circular …