API VERSION: 1.2 API SOURCE: NASA/JPL Horizons API ******************************************************************************* JPL/HORIZONS 129P/Shoemaker-Levy 3 2024-May-16 19:52:33 Rec #:90001042 (+COV) Soln.date: 2024-May-07_15:49:09 # obs: 705 (2002-2024) IAU76/J2000 helio. ecliptic osc. elements (au, days, deg., period=Julian yrs): EPOCH= 2456387.5 ! 2013-Apr-05.0000000 (TDB) RMSW= n.a. EC= .09260045646485718 QR= 3.913426347770706 TP= 2456696.034907816 OM= 185.3452219706538 W= 308.6387255000418 IN= 3.432081540619898 A= 4.31279294292387 MA= 326.0476007550724 ADIST= 4.712159538077035 PER= 8.9566605377969 N= .110043948 ANGMOM= .035570561 DAN= 4.0421 DDN= 4.53821 L= 134.0341219 B= -2.6801686 MOID= 2.92914009 TP= 2014-Feb-07.5349078160 Comet physical (GM= km^3/s^2; RAD= km): GM= n.a. RAD= n.a. M1= 14.3 M2= n.a. k1= 4.5 k2= n.a. PHCOF= n.a. Comet non-gravitational force model (AMRAT=m^2/kg;A1-A3=au/d^2;DT=days;R0=au): AMRAT= 0. DT= 0. A1= 1.312856376171E-9 A2= -2.522451430559E-10 A3= 0. Non-standard or simulated/proxy model: ALN= .04083733261 NK= 2.6 NM= 2. NN= 3. R0= 5. COMET comments 1: soln ref.= JPL#K223/29, data arc: 2002-11-04 to 2024-05-07 2: k1=4.5;Nongrav. accels. using CO driven g(r) ******************************************************************************* ******************************************************************************* Ephemeris / API_USER Thu May 16 19:52:33 2024 Pasadena, USA / Horizons ******************************************************************************* Target body name: 129P/Shoemaker-Levy 3 {source: JPL#K223/29} Center body name: Earth (399) {source: DE441} Center-site name: GEOCENTRIC ******************************************************************************* Start time : A.D. 2031-Nov-05 00:00:00.0000 UT Stop time : A.D. 2031-Nov-06 00:00:00.0000 UT Step-size : 180 minutes ******************************************************************************* Target pole/equ : undefined Target radii : undefined Center geodetic : 0.0, 0.0, -6378.137 {E-lon(deg),Lat(deg),Alt(km)} Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)} Center pole/equ : ITRF93 {East-longitude positive} Center radii : 6378.137, 6378.137, 6356.752 km {Equator_a, b, pole_c} Target primary : Sun Vis. interferer : MOON (R_eq= 1737.400) km {source: DE441} Rel. light bend : Sun {source: DE441} Rel. lght bnd GM: 1.3271E+11 km^3/s^2 Small-body perts: Yes {source: SB441-N16} Atmos refraction: NO (AIRLESS) RA format : HMS Time format : CAL Calendar mode : Mixed Julian/Gregorian EOP file : eop.240516.p240809 EOP coverage : DATA-BASED 1962-JAN-20 TO 2024-MAY-16. PREDICTS-> 2024-AUG-08 Units conversion: 1 au= 149597870.700 km, c= 299792.458 km/s, 1 day= 86400.0 s Table cut-offs 1: Elevation (-90.0deg=NO ),Airmass (>38.000=NO), Daylight (NO ) Table cut-offs 2: Solar elongation ( 0.0,180.0=NO ),Local Hour Angle( 0.0=NO ) Table cut-offs 3: RA/DEC angular rate ( 0.0=NO ) ******************************************************************************* Initial IAU76/J2000 heliocentric ecliptic osculating elements (au, days, deg.): EPOCH= 2456387.5 ! 2013-Apr-05.0000000 (TDB) RMSW= n.a. EC= .09260045646485718 QR= 3.913426347770706 TP= 2456696.034907816 OM= 185.3452219706538 W= 308.6387255000418 IN= 3.432081540619898 Equivalent ICRF heliocentric cartesian coordinates (au, au/d): X=-2.427095928814638E-01 Y= 3.746607914438783E+00 Z= 1.363849817038732E+00 VX=-8.857889929692522E-03 VY=-9.605657670795436E-04 VZ=-4.026145255936972E-04 Comet physical (GM= km^3/s^2; RAD= km): GM= n.a. RAD= n.a. M1= 14.3 M2= n.a. k1= 4.5 k2= n.a. PHCOF= n.a. Comet non-gravitational force model (AMRAT=m^2/kg;A1-A3=au/d^2;DT=days;R0=au): AMRAT= 0. DT= 0. A1= 1.312856376171E-9 A2= -2.522451430559E-10 A3= 0. Non-standard or simulated/proxy model: ALN= .04083733261 NK= 2.6 NM= 2. NN= 3. R0= 5. ******************************************************************************* Date__(UT)__HR:MN r rdot ************************************************** $$SOE 2031-Nov-05 00:00 3.933368730603 -0.0015411 2031-Nov-05 03:00 3.933368631931 -0.0011922 2031-Nov-05 06:00 3.933368558449 -0.0008433 2031-Nov-05 09:00 3.933368510155 -0.0004945 2031-Nov-05 12:00 3.933368487050 -0.0001456 2031-Nov-05 15:00 3.933368489134 0.0002033 2031-Nov-05 18:00 3.933368516406 0.0005522 2031-Nov-05 21:00 3.933368568866 0.0009010 2031-Nov-06 00:00 3.933368646515 0.0012499 $$EOE ******************************************************************************* Column meaning: TIME Times PRIOR to 1962 are UT1, a mean-solar time closely related to the prior but now-deprecated GMT. Times AFTER 1962 are in UTC, the current civil or "wall-clock" time-scale. UTC is kept within 0.9 seconds of UT1 using integer leap-seconds for 1972 and later years. Conversion from the internal Barycentric Dynamical Time (TDB) of solar system dynamics to the non-uniform civil UT time-scale requested for output has not been determined for UTC times after the next July or January 1st. Therefore, the last known leap-second is used as a constant over future intervals. Time tags refer to the UT time-scale conversion from TDB on Earth regardless of observer location within the solar system, although clock rates may differ due to the local gravity field and no analog to "UT" may be defined for that location. Any 'b' symbol in the 1st-column denotes a B.C. date. First-column blank (" ") denotes an A.D. date. CALENDAR SYSTEM Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15 (if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any) are in the Julian calendar system, which is automatically extended for dates prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for matching historical dates. The Gregorian calendar more accurately corresponds to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is available if such physical events are the primary interest. NOTE: "n.a." in output means quantity "not available" at the print-time. 'r rdot' = The Sun's apparent range ("r", light-time aberrated) and range-rate ("rdot") relative to the target center, as seen by the observer. A positive "rdot" means the target center was moving away from the Sun, negative means moving toward the Sun. Units: AU and KM/S Computations by ... Solar System Dynamics Group, Horizons On-Line Ephemeris System 4800 Oak Grove Drive, Jet Propulsion Laboratory Pasadena, CA 91109 USA General site: https://ssd.jpl.nasa.gov/ Mailing list: https://ssd.jpl.nasa.gov/email_list.html System news : https://ssd.jpl.nasa.gov/horizons/news.html User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x API https://ssd-api.jpl.nasa.gov/doc/horizons.html command-line telnet ssd.jpl.nasa.gov 6775 e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/hrzn_batch.txt scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS Author : Jon.D.Giorgini@jpl.nasa.gov *******************************************************************************