Project home: Ryugu-00.zip
Author: francisdrake
Current version: 00
Compatibility: Orbiter 2016
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Ryugu
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Ryugu in Orbiter
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Designation
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Name |
Ryugu
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Reference body |
Sun
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Number of satellites |
0
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Planetary mean orbits
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Epoch |
2020.9596167
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Semimajor axis (a) |
1.78107351195385×1011 km (1.19057410625364 AU)
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Eccentricity (e) |
0.1909944
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Inclination (i) |
0.102690286265441 radian (5.88372°)
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Longitude of the ascending node (LAN, ☊) |
0 radian 0°
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Rotational Elements
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Sidereal Rotation Period |
87133.4717273712 seconds (1.00848925610383 days)
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Sidereal Rotation Offset |
0
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Selected physical parameters
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Mean radius |
450 m
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Mass |
7.24641539269111×10<su>10 kg
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Equatorial gravity |
0.0000239 m/s-10
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Escape velocity |
0.000147 m/s
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Gravity at surface |
Ryugu 1% Sun 99%
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Note |
*Elements given are from Ryugu.cfg file.
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162173 Ryugu or in Orbiter simply Ryugu is near-Earth object of the Appolo group of small bodies, discovered by Lincoln Near-Earth Asteroid Research astronomers on 10 May 1999.
Ryugu is an add-on by francisdrake released in 2023 on the forum, and is compatible with Orbiter 2016. In Orbiter, Ryugu orbits the Sun with a semi-major axis of 1.19 AU, inclination of 0.1027 radians, and eccentricity of 0.19. Its gravity is very weak, even at the surface, in OrbitMFD, Ryugu's gravity is 1% and the Sun's gravity is 99%. A person could literally jump at greater than escape speed. Rotation is just over a day.
The landing surface (hard radius) is well inside the mesh/texture, so, landing on Ryugu places the spacecraft well inside the body.
Gallery
Orbits of the inner planets showing the orbit of Ryugu in white. From Wikimedia commons.