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111 lines
5.4 KiB
Plaintext
111 lines
5.4 KiB
Plaintext
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Revised: Jul 11, 2019 EM-L4 3014
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(Earth-Moon Lagrange 4)
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#1) The Earth-Moon Lagrange-4 point (EM-L4) is a location where the Moon's
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gravitational field partially counters that of the Earth. EM-L4 is one
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of the stable "Trojan" points (along with EM-L5). Small perturbations
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can displace an object from EM-L4, but it can return to the stable
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point.
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#2) EM-L4 lies 60 degrees ahead of the Earth-Moon system along the Moon's
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orbit in plane of the orbit. It is about 1 lunar distance from the
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Earth and from the Moon (straight-lines), so 356000 to 407000 km,
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averaging 385000 km from Earth and Moon centers, forming the apex of
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an equilateral triangle, with the Earth and Moon defining the base-line.
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Time-span available: 1900-Jan-01 to 2151-Jan-01
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Ephemeris / WWW_USER Thu Feb 17 18:31:54 2022 Pasadena, USA / Horizons
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Target body name: EM-L4 (3014) {source: Earth-Moon_L4}
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Center body name: Earth (399) {source: DE441}
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Center-site name: BODY CENTER
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Start time : A.D. 2020-Mar-24 06:00:00.0000 TDB
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Stop time : A.D. 2020-Mar-25 06:00:00.0000 TDB
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Step-size : 1440 minutes
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Center geodetic : 0.00000000,0.00000000,0.0000000 {E-lon(deg),Lat(deg),Alt(km)}
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Center cylindric: 0.00000000,0.00000000,0.0000000 {E-lon(deg),Dxy(km),Dz(km)}
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Center radii : 6378.1 x 6378.1 x 6356.8 km {Equator, meridian, pole}
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Output units : AU-D
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Output type : GEOMETRIC cartesian states
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Output format : 2 (position and velocity)
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EOP file : eop.220216.p220512
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EOP coverage : DATA-BASED 1962-JAN-20 TO 2022-FEB-16. PREDICTS-> 2022-MAY-11
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Reference frame : ICRF
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JDTDB
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X Y Z
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VX VY VZ
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$$SOE
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2458932.750000000 = A.D. 2020-Mar-24 06:00:00.0000 TDB
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X = 1.262170577138596E-03 Y = 2.254660738885763E-03 Z = 8.439158665950467E-04
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VX=-4.935321457947509E-04 VY= 2.245912867279576E-04 VZ= 1.436629421560135E-04
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2458933.750000000 = A.D. 2020-Mar-25 06:00:00.0000 TDB
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X = 7.445211227239128E-04 Y = 2.427928910875577E-03 Z = 9.679787398326978E-04
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VX=-5.378861860962063E-04 VY= 1.206328432960384E-04 VZ= 1.035202699747598E-04
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$$EOE
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TIME
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Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
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continuous relativistic coordinate time is equivalent to the relativistic
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proper time of a clock at rest in a reference frame comoving with the
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solar system barycenter but outside the system's gravity well. It is the
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independent variable in the solar system relativistic equations of motion.
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TDB runs at a uniform rate of one SI second per second and is independent
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of irregularities in Earth's rotation.
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Calendar dates prior to 1582-Oct-15 are in the Julian calendar system.
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Later calendar dates are in the Gregorian system.
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REFERENCE FRAME AND COORDINATES
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International Celestial Reference Frame (ICRF)
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The ICRF is an adopted reference frame whose axes are defined relative to
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fixed extragalactic radio sources distributed across the sky.
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The ICRF was aligned with the prior FK5/J2000 dynamical system at the ~0.02
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arcsecond level but is not identical and has no associated standard epoch.
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Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
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JDTDB Julian Day Number, Barycentric Dynamical Time
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X X-component of position vector (au)
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Y Y-component of position vector (au)
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Z Z-component of position vector (au)
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VX X-component of velocity vector (au/day)
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VY Y-component of velocity vector (au/day)
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VZ Z-component of velocity vector (au/day)
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ABERRATIONS AND CORRECTIONS
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Geometric state vectors have NO corrections or aberrations applied.
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Computations by ...
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Solar System Dynamics Group, Horizons On-Line Ephemeris System
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4800 Oak Grove Drive, Jet Propulsion Laboratory
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Pasadena, CA 91109 USA
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General site: https://ssd.jpl.nasa.gov/
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Mailing list: https://ssd.jpl.nasa.gov/email_list.html
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System news : https://ssd.jpl.nasa.gov/horizons/news.html
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User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
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Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
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API https://ssd-api.jpl.nasa.gov/doc/horizons.html
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command-line telnet ssd.jpl.nasa.gov 6775
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e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/hrzn_batch.txt
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scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
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Author : Jon.D.Giorgini@jpl.nasa.gov
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