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单词 Orbital eccentricity
释义

Orbital eccentricity

原声例句
科学大揭秘

Or, technically speaking, what is their orbital eccentricity?

或者,更准备的来说是它们的轨道偏心率是多少?

科学大揭秘

Well, then all depends on the orbital eccentricity that the planets possess.

这就取决于行星的轨道偏心率了。

科学大揭秘

For planetary objects, when orbital eccentricity crosses 1, the planet no longer remains confined to the star it is bound to and " escapes" from its gravitational influence.

对于行星状物体,当轨道偏心率超过1时,行星不再局限于它所依附的恒星,并“逃离”其引力的影响。

中文百科

轨道离心率

各种不同离心率的轨道范例,中间黑点为焦点(之一),为中心天体所在的位置。
An elliptic, parabolic and hyperbolic Kepler orbit:
      elliptic (eccentricity = 0.7)
      parabolic (eccentricity = 1)
      hyperbolic orbit (eccentricity = 1.3)
Gravity Simulator plot of the changing orbital eccentricity of Mercury, Venus, Earth, and Mars over the next 50,000 years. The arrows indicate the different scales used. The 0 point on this plot is the year 2007.
Une ellipse avec ses axes, son centre, un foyer et la droite directrice associée . a est le demi grand-axe, b est le demi petit-axe, c est la distance entre le centre O de l'ellipse et un foyer F. Pour information h est la longueur séparant le foyer F de sa directrice (d) , et h = b² / c

在天文动力学,架构在标准假说下的任何轨道都必须是圆锥切面的形状。圆锥切面的离心率,轨道离心率是定义轨道形状的重要参数,而且定义了绝对的形状。离心率可以解释为形状从圆形偏离了多少的程度。

架构在标准假说下,离心率(偏心率,e\,\!)是严格的定义了圆、椭圆、抛物线和双曲线,并且有如下的数值:

椭圆的离心率e是圆的角度投映。例如说,水星的离心率是(0.2056),简单的计算正弦的反函数可以得到投映的角度是11.86度,然后以那个数值的倾斜角度观察任何的圆形物体(例如从上面观看的咖啡杯),投射到你的眼中所看见的椭圆就会有相同的离心率。

英语百科

Orbital eccentricity 轨道离心率

An elliptic, parabolic and hyperbolic Kepler orbit:
      elliptic (eccentricity = 0.7)
      parabolic (eccentricity = 1)
      hyperbolic orbit (eccentricity = 1.3)
Gravity Simulator plot of the changing orbital eccentricity of Mercury, Venus, Earth, and Mars over the next 50,000 years. The arrows indicate the different scales used. The 0 point on this plot is the year 2007.

The orbital eccentricity of an astronomical object is a parameter that determines the amount by which its orbit around another body deviates from a perfect circle. A value of 0 is a circular orbit, values between 0 and 1 form an elliptical orbit, 1 is a parabolic escape orbit, and greater than 1 is a hyperbola. The term derives its name from the parameters of conic sections, as every Kepler orbit is a conic section. It is normally used for the isolated two-body problem, but extensions exist for objects following a rosette orbit through the galaxy.

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更新时间:2025/6/17 10:31:44