List of videos by 20 years: An Orbiter Documentary
Jump to navigation
Jump to search
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 | |
Mean radius | |
Mass | |
Density | |
Sidereal rotation period | |
Sidereal orbit period | |
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 | |
---|---|
Sun in Orbiter | |
Designation | |
Name | Sun |
Selected physical parameters | |
Equatorial gravity | |
Escape velocity | |
Note | *Elements given are from Orbiter 2016 |
Mercury
Venus
Earth
Mars
Jupiter
Saturn
Uranus
Neptune
Pluto
NoneTemplate | |
---|---|
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) | 0.24880766 |
Inclination (i) | 17.14175° (0.299180 radian) |
Longitude of the ascending node (LAN, ☊) | 110.30347° (1.925159 radian) |
Longitude of periapsis (ϖ) | 224.06676° (3.910703 radian) |
Mean longitude (L) | 238.92881° (4.170094 radian) |
Planetary orbital element centennial rates | |
Semimajor axis (a) | -0.00076912 AU/Century |
Eccentricity (e) | 0.00006465 Century-1 |
Inclination (i) | 11.07 seconds/Century |
Longitude of the ascending node (LAN, ☊) | -37.33 seconds/Century |
Longitude of periapsis (ϖ) | -132.25 seconds/Century |
Mean longitude (L) | 522747.90 seconds/Century |
Selected physical parameters | |
Mean radius | 1151 km |
Mass | 1.5×1022 kg |
Density | 1.1 g/cm3 |
Sidereal rotation period | 153.28 hours |
Sidereal orbit period | 248.0208 years |
Magnitude V(1,0) | -1.0 |
Geometric albedo | 0.3 |
Equatorial gravity | 0.655 m/s2 |
Escape velocity | 1.3 km/s |
Rotation elements | |
North pole right ascension (α1) | 311.50° |
North pole declination (δ1) | 4.14° |
Obliqutiy of ecliptic | 68.69° |
Longitude of Sun's transit | 225.19° |
Atmospheric parameters | |
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 |