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− | {| cellpadding="2" cellspacing="0" style="margin:25px 0 0 10px; border:3px solid lightsteelblue;width:250px; font-size: | + | {| cellpadding="2" cellspacing="0" style="margin:25px 0 0 10px; border:3px solid lightsteelblue;width:250px; font-size:90%; font-family:'Arial','Helvetica'; float: right; clear: right;"Template in Orbiter" |
!bgcolor="lightsteelblue" colspan="2" align="center" |Mercury | !bgcolor="lightsteelblue" colspan="2" align="center" |Mercury | ||
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|Name||align="right"|Mercury | |Name||align="right"|Mercury | ||
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− | |Reference body||align="right"|Sun | + | |width="30%"|Reference body||align="right" width="30%"|Sun |
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− | |Number of satellites||align="right" width="30%"|0 | + | |width="30%"|Number of satellites||align="right" width="30%"|0 |
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− | !bgcolor="lightsteelblue" colspan="2"|Planetary mean | + | !bgcolor="lightsteelblue" colspan="2"|Planetary mean orbits |
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− | |Epoch||align="right"|J2000 (1 January 2000) | + | |width="30%"|Epoch||align="right" width="50%"|J2000 (1 January 2000) |
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− | |Semimajor axis (a)||align="right" |0.38709893 AU <br> 5.790917567×10<sup>7</sup> km) | + | |width="30%"|Semimajor axis (a)||align="right" width="50%"|0.38709893 AU <br> 5.790917567×10<sup>7</sup> km) |
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− | |Eccentricity (e)||align="right"|0.20563069 | + | |width="30%"|Eccentricity (e)||align="right" width="30%"|0.20563069 |
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− | |Inclination (i)||align="right"|7.00487° <br> (0.122258 radian) | + | |width="30%"|Inclination (i)||align="right" width="30%"|7.00487° <br> (0.122258 radian) |
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− | |Longitude of the ascending node (LAN, ☊)||align="right"|48.33167° <br> (0.8436468 radian) | + | |width="30%"|Longitude of the ascending node (LAN, ☊)||align="right" width="30%"|48.33167° <br> (0.8436468 radian) |
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− | |Longitude of periapsis (ϖ)||align="right"|77.45645° <br> (1.351870 radian) | + | |width="30%"|Longitude of periapsis (ϖ)||align="right" width="30%"|77.45645° <br> (1.351870 radian) |
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− | |Mean longitude (L)||align="right"|252.25084° <br> (4.402608 radian) | + | |width="30%"|Mean longitude (L)||align="right" width="30%"|252.25084° <br> (4.402608 radian) |
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!bgcolor="lightsteelblue" colspan="2"|Planetary orbital element centennial rates | !bgcolor="lightsteelblue" colspan="2"|Planetary orbital element centennial rates | ||
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− | |Semimajor axis (a)||align="right"|0.00000066 AU/Century | + | |width="30%"|Semimajor axis (a)||align="right" width="50%"|0.00000066 AU/Century |
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− | |Eccentricity (e)||align="right"|0.00002527 Century<sup>-1</sup> | + | |width="30%"|Eccentricity (e)||align="right" width="50%"|0.00002527 Century<sup>-1</sup> |
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− | |Inclination (i)||align="right"|-23.51 seconds/Century | + | |width="30%"|Inclination (i)||align="right" width="30%"|-23.51 seconds/Century |
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− | |Longitude of the ascending node (LAN, ☊)||align="right"|-446.30 seconds/Century | + | |width="30%"|Longitude of the ascending node (LAN, ☊)||align="right" width="30%"|-446.30 seconds/Century |
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− | |Longitude of periapsis (ϖ)||align="right"|573.57 seconds/Century | + | |width="30%"|Longitude of periapsis (ϖ)||align="right" width="30%"|573.57 seconds/Century |
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− | |Mean longitude (L)||align="right"|538101628.29 seconds/Century | + | |width="30%"|Mean longitude (L)||align="right" width="30%"|538101628.29 seconds/Century |
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!bgcolor="lightsteelblue" colspan="2"|Selected physical parameters | !bgcolor="lightsteelblue" colspan="2"|Selected physical parameters | ||
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− | |width="30%"|Mean radius||align="right"|2440 km | + | |width="30%"|Mean radius||align="right" width="30%"|2440 km |
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− | |Mass||align="right"|3.301880×10<sup>23</sup> kg | + | |width="30%"|Mass||align="right" width="30%"|3.301880×10<sup>23</sup> kg |
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− | |Density||align="right"|5.427 g/cm<sup>3</sup> | + | |width="30%"|Density||align="right" width="30%"|5.427 g/cm<sup>3</sup> |
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− | |Sidereal rotation period||align="right"|1407.509 hours | + | |width="30%"|Sidereal rotation period||align="right" width="30%"|1407.509 hours |
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− | |Sidereal orbit period||align="right"|0.2408445 years | + | |width="30%"|Sidereal orbit period||align="right" width="30%"|0.2408445 years |
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− | |Magnitude V(1,0)||align="right"|-0.42 | + | |width="30%"|Magnitude V(1,0)||align="right" width="30%"|-0.42 |
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− | |Geometric albedo||align="right"|0.106 | + | |width="30%"|Geometric albedo||align="right" width="30%"|0.106 |
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− | |Equatorial gravity||align="right"|3. | + | |width="30%"|Equatorial gravity||align="right" width="30%"|3.701 m/s<sup>2</sup> |
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− | | | + | |width="30%"|Escape velocity||align="right" width="30%"|4.435 km/s |
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− | |Escape velocity||align="right"|4.435 km/s | ||
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!bgcolor="lightsteelblue" colspan="2"|Rotation elements | !bgcolor="lightsteelblue" colspan="2"|Rotation elements | ||
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− | |North pole right ascension (α<sub>1</sup>)||align="right"|280.99° | + | |width="30%"|North pole right ascension (α<sub>1</sup>)||align="right" width="30%"|280.99° |
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− | |North pole declination (δ<sub>1</sup>)||align="right"|61.44° | + | |width="30%"|North pole declination (δ<sub>1</sup>)||align="right" width="30%"|61.44° |
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− | | | + | |width="30%"|Obliqutiy of ecliptic||align="right" width="30%"|7.01° |
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− | |Longitude of Sun's transit||align="right"|228.31° | + | |width="30%"|Longitude of Sun's transit||align="right" width="30%"|228.31° |
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− | |Note||align="right"|*Elements given are from Orbiter.pdf (2016) | + | |width="30%"|Note||align="right" width="30%"|*Elements given are from Orbiter.pdf (2016) |
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− | '''Mercury''' is the smallest planet in the [[Solar system|solar system]] and is the closest to the [[Sun|sun]]. Mercury is a rocky planet appearing much like the [[Moon|moon]] and has virtually no atmosphere (none is modeled in Orbiter), and has no natural satellites | + | |
+ | '''Mercury''' is the smallest planet in the [[Solar system|solar system]] and is the closest to the [[Sun|sun]]. Mercury is a rocky planet appearing much like the [[Moon|moon]] and has virtually no atmosphere (none is modeled in Orbiter), and has no natural satellites. | ||
Mercury was visited in 1974 and 1975 by Mariner 10 in two flybys and was again visited by MESSENGER spacecraft orbiting Mercury from 2011 to 2015 when it was deorbited. BepiColombo, a joint mission by the European Space Ageny (ESA) and Japan Aerospace Exploraation Agency (JAXA) was launched on 20 October 2018 and is scheduled to reach Mercury on 5 December 2025. | Mercury was visited in 1974 and 1975 by Mariner 10 in two flybys and was again visited by MESSENGER spacecraft orbiting Mercury from 2011 to 2015 when it was deorbited. BepiColombo, a joint mission by the European Space Ageny (ESA) and Japan Aerospace Exploraation Agency (JAXA) was launched on 20 October 2018 and is scheduled to reach Mercury on 5 December 2025. | ||
== Orbital characteristics == | == Orbital characteristics == | ||
− | Mercury is the innermost planet in the system with a semimajor axis of 5.79×10<sup>7</sup> km. But, the orbital eccentricity is the largest of all the planets, about 0.2056, its distance ranging from 46 million to almost 70 million km from the Sun, and the inclination of its orbit is just over 7°, also largest of all the planets | + | Mercury is the innermost planet in the system with a semimajor axis of 5.79×10<sup>7</sup> km. But, the orbital eccentricity is the largest of all the planets, about 0.2056, its distance ranging from 46 million to almost 70 million km from the Sun, and the inclination of its orbit is just over 7°, also largest of all the planets. |
== Physical characteristics == | == Physical characteristics == | ||
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CAUTION! It is to be noted by pilots flying close to the ground at Mercury when approaching the North and South poles. If the vessel crosses either pole at low altitude and any great speed, errors in the simulator causes the scenario to freeze and may cause Crash to Desktop. However, if the pole is approached at very low speed, perhaps one or a few meters per second, the vessel can pass over and even land at the pole. | CAUTION! It is to be noted by pilots flying close to the ground at Mercury when approaching the North and South poles. If the vessel crosses either pole at low altitude and any great speed, errors in the simulator causes the scenario to freeze and may cause Crash to Desktop. However, if the pole is approached at very low speed, perhaps one or a few meters per second, the vessel can pass over and even land at the pole. | ||
− | + | When grounded or flying low, the DeltaGlider headlight does not light up the ground. | |
== Add-ons == | == Add-ons == | ||
===== Topography and Textures ===== | ===== Topography and Textures ===== | ||
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*[https://www.orbiter-forum.com/resources/planet-mercury-level-8-high-resolution-surface.3449/ Planet Mercury Level 8 High Resolution Surface] released 19 October 2004 by BigJimW providing level 8 textures for Mercury. | *[https://www.orbiter-forum.com/resources/planet-mercury-level-8-high-resolution-surface.3449/ Planet Mercury Level 8 High Resolution Surface] released 19 October 2004 by BigJimW providing level 8 textures for Mercury. | ||
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*[[w:Mariner 10|Mariner 10 mission]] at Wikipedia | *[[w:Mariner 10|Mariner 10 mission]] at Wikipedia | ||
*[[w:MESSENGER|MESSENGER mission]] at Wikipedia | *[[w:MESSENGER|MESSENGER mission]] at Wikipedia | ||
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== References == | == References == | ||
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{{Planet-Stub}} | {{Planet-Stub}} | ||
− | [[Category:Articles | + | [[Category: Articles]] |
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[[Category:Solar System]] | [[Category:Solar System]] | ||
[[Category: Planets]] | [[Category: Planets]] |