Above the geostationary orbit at 35,796 km altitude above the equator is a belt 230 km called "graveyard orbit" or "orbit trash" is the cemetery of satellites end of life. -- No.
-- No.
Therefore the moon must not be in a geosynchronous orbit.
The radius of the geosynchronous orbit is somewhere around 22,000 miles. The orbit's inclination and eccentricity may not necessarily be zero. The geostationary orbit is a geosynchronous orbit, which has an inclination and a zero eccentricity. -- No. All geostationary satellites are geosynchronous. A geosynchronous orbit is a high Earth orbit that allows satellites to match Earth's rotation. A Geostationary Orbit (GSO) is a geosynchronous orbit with an inclination of zero, meaning, it lies on the equator. GEO: geosynchronous earth orbit, seven earth radii, one-ninth of the distance to the moon, altitude = 36,000 km Arthur C. Clarke: In 1945, while still in his late 20s, he was the first to propose the concept of using a network of satellites in the geosynchronous orbit for television and telecommunications The radius of the geosynchronous orbit is somewhere around 22,000 miles. Therefore the moon must not be in a geosynchronous orbit. Therefore the moon must not be in a geosynchronous orbit. The Moon is now 384,000 km away from Earth. The orbital period of a geosynchronous satellite is a sidereal day, i.e., 23 hours, 56 minutes and 4 seconds, which is why it seems to stay in place over a single longitude (although it may drift south/north depending upon the orbit’s inclination with Earth’s equatorial plane). However, a new organization, called the Space Development Agency, has its gaze focused even farther out: on everything between geosynchronous orbit and the Moon. In astronomy, lunar orbit (also known as a selenocentric orbit) is the orbit of an object around the Moon. The underlying principle of the orbit is closely related to gravity, and it was not clearly explained until newton’s theory of gravity was published. Does that mean the moon approximated a geosynchronous orbit for a time on its journey outward to its current orbit? Because the radius and period are related, you can use physics to calculate one if you know the other. Geosynchronous orbit (GSO): An orbit around the Earth with a period equal to one sidereal day, which is Earth's average rotational period of 23 hours, 56 minutes, 4.091 seconds. As used in the space program, this refers not to the orbit of the Moon about the Earth, but to orbits by various manned or unmanned spacecraft around the Moon. I recognize because of the Earth's tilt of 6.7 degrees the Moon does not orbit around the Earth's equator and therefore a geostationary orbit wasn't possible. The moon does appear to move westward in the sky. Anomalies in Earth's gravitational field combined with the tug of the Moon cause all geosats to drift unless repositioned by thrusters.
The Moon orbits Earth in the prograde direction and completes one revolution relative to the stars in about 27.32 days (a sidereal month) and one revolution relative to the Sun in about 29.53 days (a synodic month).Earth and the Moon orbit about their barycentre (common center of mass), which lies about 4,600 km (2,900 mi) from Earth's center (about 72% of its radius). Geosynchronous vs Geostationary Orbit . The period of a satellite is the time it takes […] The radius of the geosynchronous orbit is somewhere around 22,000 miles. When a satellite travels in a geosynchronous orbit around the Earth, it needs to travel at a certain orbiting radius and period to maintain this orbit. An orbit is a curved path in space, in which celestial objects tend to rotate. An orbit used by communications satellites is a high Earth orbit called "geostationary" or "geosynchronous" orbit, where it takes exactly 24 hours for one orbit. A Geosynchonous Orbit (GEO) takes a satellite around the Earth at a rate of once per day, keeping it roughly in the same area over the ground. Since the Earth rotates once per 24 hours, each satellite stays "stationary" or "synchronized" above one point on Earth. Geosynchronous satellites' orbits are slightly inclined and describe a north-south-inclined figure-8 or analemma during the course of the day. For a nearly circular orbit, this implies an altitude of approximately 35,786 kilometers (22,236 mi).