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cuz my dik is big
The Earths orbit is fairly un-eccentric when compared to the other planets, with only Neptune and Venus having more regular (less eccentric) orbits. The eccentricity of earths orbit is 0.0167, the closest to this is Neptune's, with a value of 0.00859
surely a rocket or artificial satellite can get out with help of escape velocity....
Hydrogen and helium
The Earths orbital distance from the sun is 149,597,890km (92,955,820 miles) on average, enough to fit 107 more suns between the suns surface and Earth.
the suns gravitational pull is strongest because the earth is at its closest point to the sun.
Weathering
elliptical.
Earths orbital inclination is 1.57869°
The year.
cuz my dik is big
they pull toward each other, but the earths orbital velocity compensates exactly for this acceleration together due to gravity a = (G* (m1+m2))/d^2 acceleration that balances this a = v^2/d : G = newtons gravitational constant m1 = sun mass m2 = earth mass d = distance between centres v = orbital velocity
gravity
At lower speed, the object will fall back on the ground. Since, earth is curved, if the object has enought speed, the object can try to fall beyond the curvature of the earth. Thus, it will not hit ground at all. The speed to achieve it is around 8 km/s. If the object is faster than 11.4 km/s then the object will never return. It is called escape velocity.
Aphelion is 152,098,232 km (the distance when the Earth is furthest from the Sun in July) at that point it is moving slowest: 29,300 m/s. Perihelion is 147,098,290 km (in January when the Earth is closest to the Sun) the orbital speed is greatest: 30,300 m/s.
(simplified) Gravitational force of attraction is balanced by centripital force due to earths velocity. (G*m1*m2) / r2 = m2 * (v2 / r) m1 = sun mass m2 = earth mass r = earth - sun distance v = earths orbital velocity G = newtons gravitational constant
In astronomy, axial tilt, also known as obliquity, is the angle between an object's rotational axis and its orbital axis, or, equivalently, the angle between its equatorial plane and orbital plane. It differs from orbital inclination.