Template:Infobox planet/doc

This template has been designed for the presentation of information on non-stellar astronomical bodies: planets (including extrasolar planets), dwarf planets, moons and minor planets. Some parameters will not be applicable to individual types; these may be omitted without any problems to the template's function.

Usage notes

 * This template expects that the tag will be present in articles setting the minorplanet parameter to yes. Pages without a  tag  will show Cite error: There are tags on this page for a group named "note", but the references will not show without a   tag; see Help:Cite errors. at the bottom of the page.
 * When parameters relating to minor planets are used (e.g. mp_name), several subheadings and wikilinks within the template are made specific to minor planets. For standard formulas for computable values and sources of physical data, see Template talk:Infobox Nonstellar body and Standard asteroid physical characteristics.
 * For bodies orbiting bodies other than the Sun, include the parameter |apsis = (appropriate suffix) . This will replace various parameters' default "-helion" suffix to the suffix set by the apsis parameter. For example, setting |apsis = astron converts the labels "perihelion", "aphelion" and "Argument of perihelion" into "periastron", "apastron" and "Argument of periastron" respectively.

Recommended parameters
For a list of all parameters, see All parameters below.

Exosolar planets


Minor planets


See here for means of semi-automating this template's transclusion as regards minor planets.
 * For satellites of minor planets, include the parameter |apsis = astron (see above).

All parameters


Computed values
This section documents how some minor planet parameters may be computed when they're not directly measured. More detail can be found in Standard asteroid physical characteristics.

Average orbital speed
This is very simply the orbital circumference divided by the orbital period.

The exact circumference of an ellipse is $$4 a E(e)$$, where a is the semi-major axis, e the eccentricity, and the function E is the complete elliptic integral of the second kind. This gives

v_o = \frac{4 a E(e)}{T} $$ E is close to $$ \pi / 2$$ when e is small.

An approximation using a taylor series expansion is

v_o = \frac{2\pi a}{T}\left[1-\frac{e^2}{4}-\frac{3e^4}{64} - \dots \right] $$

AstOrb Browser computes a velocity using Ramanujan's approximation for an ellipse's circumference:
 * $$v_o \approx \frac{\pi}{T} \left[3(a+b) - \sqrt{(3a+b)(a+3b)}\right] $$

Where b is the orbit's semi-minor axis:
 * $$b = a \sqrt{1-e^2}\,\!$$

Surface gravity
For a spherical body of mass m, and radius r, the gravitational acceleration at the surface, is given by


 * $$g_{\rm spherical} = \frac{GM}{r^2}\,\!$$

Where G = 6.6742 m3s-2kg-1 is the Gravitational constant, M is the mass of the body, and r its radius. This value is very approximate, as most minor planets are far from spherical.

For irregularly shaped bodies, the surface gravity will differ appreciably with location. However, at the outermost point/s, where the distance to the centre of mass is the greatest, the surface gravity is still given by a simple formula, a slightly modified version of the above that uses the largest radius $$r_{\rm max}$$


 * $$g_{\rm outer} = \frac{GM}{r_{\rm max}^2}\,.\!$$

because all the body's mass is contained within this radius.

On a rotating body, the apparent weight experienced by an object on the surface is reduced by the centrifugal force, when one is away from the poles. The centrifugal acceleration experienced at the equator is


 * $$g_{\rm centrifugal} = -\left(\frac{2\pi}{T}\right)^2 r_{\rm eq}$$

where T is the rotation period in seconds, and $$r_{\rm eq}$$ is the equatorial radius (usually also the maximum radius used above). The negative sign indicates that it acts in the opposite direction to the gravitational acceleration g.

The effective surface gravity at the equator is then


 * $$ g_{\rm effective} \approx g_{\rm gravitational} + g_{\rm centrifugal}

= g_{\rm gravitational} - |g_{\rm centrifugal}|\ .$$

Escape velocity
For surface gravity g and radius r, the escape velocity is:
 * $$v_e = \sqrt{2gr}$$

This value is much less sensitive to the factors affecting the surface gravity, mentioned above.

Temperature
For asteroid albedo &alpha;, semimajor axis a, solar luminosity $$L_0$$, and asteroid infrared emissivity &epsilon; (usually taken to be ~0.9), the approximate mean temperature T is given by:
 * $$T = \left ( \frac{(1 - \alpha) L_0}{\epsilon \sigma 16 \pi a^2} \right )^{\frac{1}{4}}$$

Where &sigma; is Stefan-Boltzmann constant. See also.