Difference between revisions of "List of videos by 20 years: An Orbiter Documentary"

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(infoboxes.)
(Tables.)
Line 1: Line 1:
 
Template
 
Template
  
−
{| 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;"Earth in Orbiter"
+
{| 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" |Earth
+
!bgcolor="lightsteelblue" colspan="2" align="center" |Template
 
|-
 
|-
−
|colspan="2" align="center"|[[Image:EarthScrshot.jpg|240px]]
+
|colspan="2" align="center"|[[Image:|240px]]
 
|-
 
|-
−
|colspan="2" align="center"|'''Earth in Orbiter'''
+
|colspan="2" align="center"|'''Template in Orbiter'''
 
|-
 
|-
 
!bgcolor="lightsteelblue" colspan="2"|Designation
 
!bgcolor="lightsteelblue" colspan="2"|Designation
 
|-
 
|-
−
|width="30%"|Name||align="right" width="30%"|Earth
+
|width="30%"|Name||align="right" width="30%"|Template
 
|-
 
|-
 
|width="30%"|Reference body||align="right" width="30%"|Sun
 
|width="30%"|Reference body||align="right" width="30%"|Sun
 
|-
 
|-
−
|width="30%"|Number of satellites||align="right" width="30%"|1
+
|width="30%"|Number of satellites||align="right" width="30%"|0
 
|-
 
|-
 
!bgcolor="lightsteelblue" colspan="2"|Orbital Characteristics*
 
!bgcolor="lightsteelblue" colspan="2"|Orbital Characteristics*
Line 65: Line 65:
 
|-
 
|-
 
|width="30%"|Mass||align="right" width="30%"|
 
|width="30%"|Mass||align="right" width="30%"|
 +
|-
 +
|width="30%"|Mean density||align="right" width="30%"|
 +
|-
 +
|width="30%"|Surface gravity||align="right" width="30%"|
 +
|-
 +
|width="30%"|Escape velocity||align="right" width="30%"|
 +
|-
 +
|width="30%"|Rotation period||align="right" width="30%"|
 +
|-
 +
|width="30%"|Sidereal rotation period||align="right" width="30%"|
 +
|-
 +
|width="30%"|Equatorial rotation velocity||align="right" width="30%"|
 +
|-
 +
|width="30%"|Axial tilt (obliquity)||align="right" width="30%"|
 +
|-
 +
|width="30%"|Right ascension north pole||align="right" width="30%"|
 +
|-
 +
|width="30%"|Declination north pole||align="right" width="30%"|
 +
|-
 +
!bgcolor="lightsteelblue" colspan="2"|Atmosphere*
 +
|-
 +
|width="30%"|Atmosphere model||align="right" width="30%"|
 +
|-
 +
|width="30%"|Surface Pressure||align="right" width="30%"|
 +
|-
 +
|width="30%"|Surface Density||align="right" width="30%"|
 +
|-
 +
|width="30%"|Specific gas constant||align="right" width="30%"|
 +
|-
 +
|width="30%"|Specific heat ratio||align="right" width="30%"|
 +
|-
 +
!bgcolor="lightsteelblue" colspan="2"|Ecliptic position from primary*
 +
|-
 +
|width="30%"|Note||align="right" width="30%"|*Elements given are from Orbiter 2016
 +
|}
 +
 +
{| 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;"Sun in Orbiter"
 +
!bgcolor="lightsteelblue" colspan="2" align="center" |Sun
 +
|-
 +
|colspan="2" align="center"|[[Image:SunScrshot.jpg|240px]]
 +
|-
 +
|colspan="2" align="center"|'''Sun in Orbiter'''
 +
|-
 +
!bgcolor="lightsteelblue" colspan="2"|Designation
 +
|-
 +
|width="30%"|Name||align="right" width="30%"|Sun
 +
|-
 +
|width="30%"|Reference body||align="right" width="30%"|None
 +
|-
 +
!bgcolor="lightsteelblue" colspan="2"|Orbital Characteristics*
 +
|-
 +
!bgcolor="lightsteelblue" colspan="2"|Physical Characteristics*
 +
|-
 +
|width="30%"|Mean radius||align="right" width="30%"|1.988919×10<sup>30</sup> kg
 +
|-
 +
|width="30%"|Equatorial radius||align="right" width="30%"|
 +
|-
 +
|width="30%"|Polar radius||align="right" width="30%"|
 +
|-
 +
|width="30%"|Flattening||align="right" width="30%"|
 +
|-
 +
|width="30%"|Surface area||align="right" width="30%"|4.971×10<sup>61</sup> km<sup>2</sup>
 +
|-
 +
|width="30%"|Volume||align="right" width="30%"|
 +
|-
 +
|width="30%"|Mass||align="right" width="30%"|6.96×10<sup>8</sup> km
 
|-
 
|-
 
|width="30%"|Mean density||align="right" width="30%"|
 
|width="30%"|Mean density||align="right" width="30%"|
Line 123: Line 189:
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|-
 
|-
−
|width="30%"|Semimajor axis||align="right" width="50%"|
+
|width="30%"|Semimajor axis||align="right" width="50%"|0.38709893 AU<br>(5.79091757×10<sup>10</sup> km)
 
|-
 
|-
−
|width="30%"|Eccentricity||align="right" width="30%"|
+
|width="30%"|Eccentricity||align="right" width="30%"|0.20563069 <br> (0.12225804 radian)
 
|-
 
|-
 
|width="30%"|Orbital period||align="right" width="30%"|
 
|width="30%"|Orbital period||align="right" width="30%"|
Line 137: Line 203:
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|-
 
|-
−
|width="30%"|Inclination||align="right" width="30%"|
+
|width="30%"|Inclination||align="right" width="30%"|7.00487° <br> (0.122258 radian)
 
|-
 
|-
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
Line 224: Line 290:
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|-
 
|-
−
|width="30%"|Semimajor axis||align="right" width="50%"|
+
|width="30%"|Semimajor axis||align="right" width="50%"|0.72333199 AU <br> (1.08208926×10<sup>11</sup> km)
 
|-
 
|-
−
|width="30%"|Eccentricity||align="right" width="30%"|
+
|width="30%"|Eccentricity||align="right" width="30%"|0.00677323
 
|-
 
|-
 
|width="30%"|Orbital period||align="right" width="30%"|
 
|width="30%"|Orbital period||align="right" width="30%"|
Line 238: Line 304:
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|-
 
|-
−
|width="30%"|Inclination||align="right" width="30%"|
+
|width="30%"|Inclination||align="right" width="30%"|3.39471° <br> (0.0592489 radian)
 
|-
 
|-
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
Line 325: Line 391:
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|-
 
|-
−
|width="30%"|Semimajor axis||align="right" width="50%"|
+
|width="30%"|Semimajor axis||align="right" width="50%"|1.00000011 AU <br> (1.49597887×10<sup>11</sup> km)
 
|-
 
|-
−
|width="30%"|Eccentricity||align="right" width="30%"|
+
|width="30%"|Eccentricity||align="right" width="30%"|0.01671022
 
|-
 
|-
 
|width="30%"|Orbital period||align="right" width="30%"|
 
|width="30%"|Orbital period||align="right" width="30%"|
Line 339: Line 405:
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|-
 
|-
−
|width="30%"|Inclination||align="right" width="30%"|
+
|width="30%"|Inclination||align="right" width="30%"|0.00005° <br> (8×10<sup>-7</sup> radian)
 
|-
 
|-
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
Line 429: Line 495:
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|-
 
|-
−
|width="30%"|Semimajor axis||align="right" width="50%"|
+
|width="30%"|Semimajor axis||align="right" width="50%"|1.52366231 AU <br> (2.27936637×10<sup>11</sup> km)
 
|-
 
|-
−
|width="30%"|Eccentricity||align="right" width="30%"|
+
|width="30%"|Eccentricity||align="right" width="30%"|0.09341233
 
|-
 
|-
 
|width="30%"|Orbital period||align="right" width="30%"|
 
|width="30%"|Orbital period||align="right" width="30%"|
Line 443: Line 509:
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|-
 
|-
−
|width="30%"|Inclination||align="right" width="30%"|
+
|width="30%"|Inclination||align="right" width="30%"|1.85061° <br> (0.0322992 radian)
 
|-
 
|-
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
Line 637: Line 703:
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|-
 
|-
−
|width="30%"|Semimajor axis||align="right" width="50%"|
+
|width="30%"|Semimajor axis||align="right" width="50%"|5.20336301 AU <br> (7.78412027×10<sup>11</sup> km)
 
|-
 
|-
−
|width="30%"|Eccentricity||align="right" width="30%"|
+
|width="30%"|Eccentricity||align="right" width="30%"|0.04839266
 
|-
 
|-
 
|width="30%"|Orbital period||align="right" width="30%"|
 
|width="30%"|Orbital period||align="right" width="30%"|
Line 651: Line 717:
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|-
 
|-
−
|width="30%"|Inclination||align="right" width="30%"|
+
|width="30%"|Inclination||align="right" width="30%"|1.60530° <br> (0.0280178 radian)
 
|-
 
|-
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
Line 750: Line 816:
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|-
 
|-
−
|width="30%"|Semimajor axis||align="right" width="50%"|
+
|width="30%"|Semimajor axis||align="right" width="50%"|9.53707032 AU <br> (1.42672541×10<sup>12</sup> km)
 
|-
 
|-
−
|width="30%"|Eccentricity||align="right" width="30%"|
+
|width="30%"|Eccentricity||align="right" width="30%"|0.05415060
 
|-
 
|-
 
|width="30%"|Orbital period||align="right" width="30%"|
 
|width="30%"|Orbital period||align="right" width="30%"|
Line 764: Line 830:
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|-
 
|-
−
|width="30%"|Inclination||align="right" width="30%"|
+
|width="30%"|Inclination||align="right" width="30%"|2.48446° <br> (0.0433620 radian)
 
|-
 
|-
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
Line 875: Line 941:
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|-
 
|-
−
|width="30%"|Semimajor axis||align="right" width="50%"|
+
|width="30%"|Semimajor axis||align="right" width="50%"|19.19126393 AU <br> (2.87097222×10<sup>12</sup> km)
 
|-
 
|-
−
|width="30%"|Eccentricity||align="right" width="30%"|
+
|width="30%"|Eccentricity||align="right" width="30%"|0.04716771
 
|-
 
|-
 
|width="30%"|Orbital period||align="right" width="30%"|
 
|width="30%"|Orbital period||align="right" width="30%"|
Line 889: Line 955:
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|-
 
|-
−
|width="30%"|Inclination||align="right" width="30%"|
+
|width="30%"|Inclination||align="right" width="30%"|0.76986° <br> (0.0134366 radian)
 
|-
 
|-
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
Line 991: Line 1,057:
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|-
 
|-
−
|width="30%"|Semimajor axis||align="right" width="50%"|
+
|width="30%"|Semimajor axis||align="right" width="50%"|30.06896348 AU <br> (4.49825291×10<sup>12</sup> km)
 
|-
 
|-
−
|width="30%"|Eccentricity||align="right" width="30%"|
+
|width="30%"|Eccentricity||align="right" width="30%"|0.00858587
 
|-
 
|-
 
|width="30%"|Orbital period||align="right" width="30%"|
 
|width="30%"|Orbital period||align="right" width="30%"|
Line 1,005: Line 1,071:
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|-
 
|-
−
|width="30%"|Inclination||align="right" width="30%"|
+
|width="30%"|Inclination||align="right" width="30%"|1.76917° <br> (0.0308778 radian)
 
|-
 
|-
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
Line 1,101: Line 1,167:
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|width="30%"|Periapsis||align="right" width="50%"|
 
|-
 
|-
−
|width="30%"|Semimajor axis||align="right" width="50%"|
+
|width="30%"|Semimajor axis||align="right" width="50%"|39.48168677 AU <br> (5.90637627×10<sup>12</sup> km)
 
|-
 
|-
−
|width="30%"|Eccentricity||align="right" width="30%"|
+
|width="30%"|Eccentricity||align="right" width="30%"|0.24880766
 
|-
 
|-
 
|width="30%"|Orbital period||align="right" width="30%"|
 
|width="30%"|Orbital period||align="right" width="30%"|
Line 1,115: Line 1,181:
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|width="30%"|Mean motion||align="right" width="30%"|
 
|-
 
|-
−
|width="30%"|Inclination||align="right" width="30%"|
+
|width="30%"|Inclination||align="right" width="30%"|17.14175° (0.299180 radian)
 
|-
 
|-
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|
 
|width="30%"|Longitude of the ascending node (LAN)||align="right" width="30%"|

Revision as of 11:41, 19 August 2021

Template

Template
[[Image:|240px]]
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites 0
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis
Eccentricity
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model
Surface Pressure
Surface Density
Specific gas constant
Specific heat ratio
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016
Sun
SunScrshot.jpg
Sun in Orbiter
Designation
Name Sun
Reference body None
Orbital Characteristics*
Physical Characteristics*
Mean radius 1.988919×1030 kg
Equatorial radius
Polar radius
Flattening
Surface area 4.971×1061 km2
Volume
Mass 6.96×108 km
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Mercury

Mercury
MercuryScrshot.jpg
Mercury in Orbiter
Designation
Name Earth
Reference body Sun
Number of known satellites 0
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis 0.38709893 AU
(5.79091757×1010 km)
Eccentricity 0.20563069
(0.12225804 radian)
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination 7.00487°
(0.122258 radian)
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Venus

Venus
VenusScrshot.jpg
Venus in Orbiter
Designation
Name Venus
Reference body Sun
Number of known satellites 0
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis 0.72333199 AU
(1.08208926×1011 km)
Eccentricity 0.00677323
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination 3.39471°
(0.0592489 radian)
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Earth

Earth
EarthScrshot.jpg
Earth in Orbiter
Designation
Name Earth
Reference body Sun
Number of satellites 1
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis 1.00000011 AU
(1.49597887×1011 km)
Eccentricity 0.01671022
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination 0.00005°
(8×10-7 radian)
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Moon


Mars

Mars
MarsScrshot.jpg
Mars in Orbiter
Designation
Name Mars
Reference body Sun
Number of known satellites 2
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis 1.52366231 AU
(2.27936637×1011 km)
Eccentricity 0.09341233
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination 1.85061°
(0.0322992 radian)
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Phobos


Deimos


Vesta

Vesta
VestaScrshot.jpg
Vesta in Orbiter
Designation
Name Vesta
Reference body Sun
Number of known satellites 0
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis
Eccentricity
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Jupiter

Jupiter
JupiterScrshot.jpg
Jupiter in Orbiter
Designation
Name Jupiter
Reference body Sun
Number of known satellites 80
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis 5.20336301 AU
(7.78412027×1011 km)
Eccentricity 0.04839266
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination 1.60530°
(0.0280178 radian)
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Io


Europa


Ganymede


Callisto


Saturn

Saturn
SaturnScrshot.jpg
Saturn in Orbiter
Designation
Name Saturn
Reference body Sun
Number of known satellites 82
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis 9.53707032 AU
(1.42672541×1012 km)
Eccentricity 0.05415060
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination 2.48446°
(0.0433620 radian)
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Mimas


Enceladus


Tethys


Dione


Rhea


Titan


Hyperion


Iapetus


Uranus

Uranus
UranusScrshot.jpg
Uranus in Orbiter
Designation
Name Uranus
Reference body Sun
Number of known satellites 27
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis 19.19126393 AU
(2.87097222×1012 km)
Eccentricity 0.04716771
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination 0.76986°
(0.0134366 radian)
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Miranda


Ariel


Umbriel


Titania


Oberon


Neptune

Neptune
NeptuneScrshot.jpg
Neptune in Orbiter
Designation
Name Neptune
Reference body Sun
Number of known satellites 14
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis 30.06896348 AU
(4.49825291×1012 km)
Eccentricity 0.00858587
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination 1.76917°
(0.0308778 radian)
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Proteus


Triton


Nereid


Pluto

Pluto
240px
Pluto in Orbiter
Designation
Name Pluto
Reference body Sun
Number of known satellites 5
Orbital Characteristics*
Apoapsis
Periapsis
Semimajor axis 39.48168677 AU
(5.90637627×1012 km)
Eccentricity 0.24880766
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Inclination 17.14175° (0.299180 radian)
Longitude of the ascending node (LAN)
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Mass
Mean density
Surface gravity
Escape velocity
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Right ascension north pole
Declination north pole
Atmosphere*
Atmosphere model J71G
Surface Pressure 101.3 KPa
Surface Density 1.225 kg/m3
Specific gas constant 286.91 J/(K kg)
Specific heat ratio 1.40
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016
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