List of videos by 20 years: An Orbiter Documentary

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Template

Template
[[Image:|240px]]
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Sun

Sun
SunScrshot.jpg
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Mercury

Template
MercuryScrshot.jpg
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a) 0.38709893 AU
5.790917567×1010 km)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Venus

Template
VenusScrshot.jpg
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a) 0.72333199 AU
(1.082089255×1011 km)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Earth

Template
EarthScrshot.jpg
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a) 1.00000011 AU
(1.495978871×1011 km)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Mars

Template
MarsScrshot.jpg
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a) 1.52366231 AU
(2.279366372×1011 km)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Jupiter

Template
JupiterScrshot.jpg
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a) 5.20336301 AU
(7.784120267×1011 km)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Saturn

Template
SaturnScrshot.jpg
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a) 9.53707032 AU
(1.426725413×1012 km)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Uranus

Template
UranusScrshot.jpg
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a) 19.19126393 AU
(2.87097222×1012 km)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Neptune

Template
NeptuneScrshot.jpg
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a) 30.06896348 AU
(4.49825291×1012 km)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016

Pluto

Template
240px
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites
Planetary mean orbits
Epoch J2000 (1 January 2000)
Semimajor axis (a) 39.48168677 AU
(5.906376272×1012 km)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Longitude of periapsis (ϖ)
Mean longitude (L)
Planetary orbital element centennial rates
Semimajor axis (a)
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊) N/A
Longitude of periapsis (ϖ)
Mean longitude (L)
Selected physical parameters
Magnitude V(1,0)
Geometric albedo
Equatorial gravity
Escape velocity
Rotation elements
North pole right ascension (α)
North pole declination (δ)
Obliqutiy of ecliptic
Longitude of Sun's transit
Atmospheric parameters
Surface Pressure
Surface Density
Scale height
Average temperature
Wind speeds
Ecliptic position from primary*
Note *Elements given are from Orbiter 2016


Template 2

Template
[[Image:|240px]]
Template in Orbiter
Designation
Name Template
Reference body Sun
Number of satellites 0
Orbital Characteristics*
Epoch J2000 (1 January 2000)
Semimajor axis (a)
Apoapsis
Periapsis
Eccentricity (e)
Inclination (i)
Longitude of the ascending node (LAN, ☊)
Orbital period
Synodic period N/A
Average orbital speed
Mean anomaly
Mean motion
Time of periapsis
Argument of periapsis
Precession Longitude of ascending node
Precession obliquity
Precession period
Physical Characteristics*
Mean radius
Mass
Mean density
Surface gravity
Escape velocity
Equatorial radius
Polar radius
Flattening
Surface area
Volume
Rotation period
Sidereal rotation period
Equatorial rotation velocity
Axial tilt (obliquity)
Longitude of Sun's transit
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