Difference between revisions of "Earth"
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|width="30%"|Reference body||align="right" width="30%"|Sun | |width="30%"|Reference body||align="right" width="30%"|Sun | ||
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| − | |width="30%"|Number of satellites||align="right" width="30%"| | + | |width="30%"|Number of satellites||align="right" width="30%"|1 |
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!bgcolor="lightsteelblue" colspan="2"|Planetary mean orbits | !bgcolor="lightsteelblue" colspan="2"|Planetary mean orbits | ||
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|width="30%"|Equatorial gravity||align="right" width="30%"|9.780327 m/s<sup>2</sup> | |width="30%"|Equatorial gravity||align="right" width="30%"|9.780327 m/s<sup>2</sup> | ||
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| + | |width="30%"|J coefficients||align="right" width="30%"|1082.6269e-6 -2.51e-6 -1.60e-6 -0.15e-6 | ||
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|width="30%"|Escape velocity||align="right" width="30%"|11.186 km/s | |width="30%"|Escape velocity||align="right" width="30%"|11.186 km/s | ||
Revision as of 18:33, 20 October 2022
| Earth | |
|---|---|
| |
| Earth in Orbiter | |
| Designation | |
| Name | Earth |
| Reference body | Sun |
| Number of satellites | 1 |
| Planetary mean orbits | |
| Epoch | J2000 (1 January 2000) |
| Semimajor axis (a) | 1.00000011 AU (1.495978871×1011 km) |
| Eccentricity (e) | 0.01671022 |
| Inclination (i) | 0.00005° (0.00000087 radian) |
| Longitude of the ascending node (LAN, ☊) | -11.26064° (-0.1965352 radian) |
| Longitude of periapsis (ϖ) | 102.94719° (1.796767 radian_ |
| Mean longitude (L) | 100.46435° (1.753434 radian) |
| Planetary orbital element centennial rates | |
| Semimajor axis (a) | -0.00000005 AU/Century |
| Eccentricity (e) | -0.00003804 Century-1 |
| Inclination (i) | -46.94 seconds/Century |
| Longitude of the ascending node (LAN, ☊) | -18228.25 seconds/Century |
| Longitude of periapsis (ϖ) | 1198.28 seconds/Century |
| Mean longitude (L) | 129597740.63 seconds/Century |
| Selected physical parameters | |
| Mean radius | 6371.01 km |
| Mass | 5.973698968×1024 kg |
| Density | 5.515 g/cm3 |
| Sidereal rotation period | 23.93447 hours |
| Sidereal orbit period | 0.9999786 years |
| Magnitude V(1,0) | -3.86 |
| Geometric albedo | 0.65 |
| Equatorial gravity | 9.780327 m/s2 |
| J coefficients | 1082.6269e-6 -2.51e-6 -1.60e-6 -0.15e-6 |
| Escape velocity | 11.186 km/s |
| Rotation elements | |
| North pole right ascension (α1) | n/a |
| North pole declination (δ1) | 90° |
| Obliqutiy of ecliptic | 23.44° |
| Longitude of Sun's transit | 0° |
| Atmospheric parameters | |
| Surface Pressure | 101.4 kPa |
| Surface Density | 1.217 kg/m3 |
| Scale height | 8.5 km |
| Average temperature | 288 K |
| Wind speeds | 0-100 m/s |
| Ecliptic position from primary* | |
| Note | *Elements given are from Orbiter.pdf (2016) |
Earth is the third planet from the Sun and is the only body known to have life. It is one of the four 'rocky' planets, the others are Mercury, Venus, and Mars. The Moon is the only natural satellite orbiting the earth.
The Earth is close to an oblate spheroid, but, in Orbiter it's modeled as a sphere, its mean diameter is 6371.01 km, but gravitational calculations include the J coefficients given in the table to the right. The sidereal day is 86164.092 seconds, the obliquity is 23.439291°.
Natural satellites
Spaceports
The stock Orbiter includes 35 bases, some of which include details such as runways, landing pads, buildings, etc, some only include a marker to depict its location.
See Listing of Earth spaceports in Orbiter2016
See also
- Spaceport, a listing of spaceports on the real Earth used to launch rockets and spacecraft.
- Earth spaceports in Orbiter2016
- Addons for Earth
- Earth at Wikipedia
External links
Earth at Wikipedia
| edit The Solar System | |
|---|---|
| Central star |
Sun (Sol) |
| Planets |
Mercury - Venus - Earth - Mars - Jupiter - Saturn - Uranus - Neptune |
| Natural satellites |
Moon - Phobos - Deimos - Io - Europa - Ganymede - Titan - more... |
| Add-ons |
Planets - Dwarf Planets - Small objects - Natural satellites - Alternative star systems |
| This article, about a planet, is a stub. You can help Orbiterwiki by expanding it.
|