******************************************************************************* JPL/HORIZONS 27 Euterpe (A853 VA) 2024-May-03 17:28:56 Rec #: 27 (+COV) Soln.date: 2024-Apr-17_17:28:44 # obs: 3604 (1853-2024) IAU76/J2000 helio. ecliptic osc. elements (au, days, deg., period=Julian yrs): EPOCH= 2457826.5 ! 2017-Mar-14.00 (TDB) Residual RMS= .24023 EC= .1728368718542225 QR= 1.941293887868899 TP= 2457378.1989034065 OM= 94.78930499152341 W= 356.6068722982138 IN= 1.583689737796241 A= 2.346929912386967 MA= 122.8920233649068 ADIST= 2.752565936905034 PER= 3.59549 N= .274128313 ANGMOM= .025956486 DAN= 1.9418 DDN= 2.75156 L= 91.3974704 B= -.0937214 MOID= .95845097 TP= 2015-Dec-21.6989034065 Asteroid physical parameters (km, seconds, rotational period in hours): GM= n.a. RAD= 48. ROTPER= 10.4082 H= 7.08 G= .150 B-V= .878 ALBEDO= .215 STYP= S ASTEROID comments: 1: soln ref.= JPL#133, OCC=0 2: source=ORB ******************************************************************************* ******************************************************************************* Ephemeris / WWW_USER Fri May 3 17:28:56 2024 Pasadena, USA / Horizons ******************************************************************************* Target body name: 27 Euterpe (A853 VA) {source: JPL#133} Center body name: Earth (399) {source: DE441} Center-site name: GEOCENTRIC ******************************************************************************* Start time : A.D. 2015-Dec-01 00:00:00.0000 UT Stop time : A.D. 2015-Dec-31 00:00:00.0000 UT Step-size : 1440 minutes ******************************************************************************* Target pole/equ : undefined Target radii : 48. km 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.240503.p240727 EOP coverage : DATA-BASED 1962-JAN-20 TO 2024-MAY-03. PREDICTS-> 2024-JUL-26 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= 2457826.5 ! 2017-Mar-14.00 (TDB) Residual RMS= .24023 EC= .1728368718542225 QR= 1.941293887868899 TP= 2457378.1989034065 OM= 94.78930499152341 W= 356.6068722982138 IN= 1.583689737796241 Equivalent ICRF heliocentric cartesian coordinates (au, au/d): X=-1.711390779696548E+00 Y=-1.827917831534161E+00 Z=-7.361517280029448E-01 VX= 6.632625386844024E-03 VY=-6.839725691508087E-03 VZ=-3.145618792335219E-03 Asteroid physical parameters (km, seconds, rotational period in hours): GM= n.a. RAD= 48. ROTPER= 10.4082 H= 7.08 G= .150 B-V= .878 ALBEDO= .215 STYP= S ************************************************************************************************************** Date__(UT)__HR:MN APmag S-brt r rdot delta deldot S-O-T /r ************************************************************************************************************** $$SOE 2015-Dec-01 00:00 9.396 4.670 1.945381179194 -0.4780717 1.02584769605969 -9.3504288 150.4095 /L 2015-Dec-02 00:00 9.366 4.652 1.945111726786 -0.4549854 1.02054442549244 -9.0135744 151.5533 /L 2015-Dec-03 00:00 9.336 4.634 1.944855616603 -0.4318714 1.01543757482758 -8.6702291 152.7061 /L 2015-Dec-04 00:00 9.305 4.615 1.944612864184 -0.4087312 1.01053087547017 -8.3204591 153.8677 /L 2015-Dec-05 00:00 9.275 4.596 1.944383484267 -0.3855661 1.00582801148948 -7.9643614 155.0377 /L 2015-Dec-06 00:00 9.244 4.576 1.944167490782 -0.3623775 1.00133260320318 -7.6020594 156.2160 /L 2015-Dec-07 00:00 9.213 4.555 1.943964896856 -0.3391668 0.99704819212320 -7.2337026 157.4024 /L 2015-Dec-08 00:00 9.181 4.534 1.943775714805 -0.3159355 0.99297822563288 -6.8594682 158.5965 /L 2015-Dec-09 00:00 9.149 4.511 1.943599956133 -0.2926849 0.98912604001376 -6.4795645 159.7981 /L 2015-Dec-10 00:00 9.118 4.488 1.943437631532 -0.2694165 0.98549484089410 -6.0942365 161.0067 /L 2015-Dec-11 00:00 9.085 4.464 1.943288750879 -0.2461316 0.98208768086879 -5.7037699 162.2221 /L 2015-Dec-12 00:00 9.053 4.440 1.943153323235 -0.2228316 0.97890743491898 -5.3084943 163.4439 /L 2015-Dec-13 00:00 9.019 4.414 1.943031356841 -0.1995181 0.97595677520360 -4.9087821 164.6717 /L 2015-Dec-14 00:00 8.986 4.387 1.942922859120 -0.1761923 0.97323814753301 -4.5050435 165.9050 /L 2015-Dec-15 00:00 8.951 4.359 1.942827836673 -0.1528558 0.97075375207581 -4.0977171 167.1434 /L 2015-Dec-16 00:00 8.916 4.330 1.942746295280 -0.1295099 0.96850553046106 -3.6872573 168.3865 /L 2015-Dec-17 00:00 8.880 4.299 1.942678239898 -0.1061561 0.96649516058239 -3.2741208 169.6338 /L 2015-Dec-18 00:00 8.843 4.266 1.942623674660 -0.0827957 0.96472405947961 -2.8587521 170.8848 /L 2015-Dec-19 00:00 8.805 4.232 1.942582602875 -0.0594303 0.96319339402775 -2.4415708 172.1392 /L 2015-Dec-20 00:00 8.765 4.195 1.942555027025 -0.0360613 0.96190409886963 -2.0229597 173.3963 /L 2015-Dec-21 00:00 8.722 4.155 1.942540948769 -0.0126900 0.96085690078207 -1.6032543 174.6557 /L 2015-Dec-22 00:00 8.676 4.110 1.942540368938 0.0106821 0.96005234800244 -1.1827368 175.9170 /L 2015-Dec-23 00:00 8.624 4.061 1.942553287539 0.0340535 0.95949084172765 -0.7616348 177.1794 /L 2015-Dec-24 00:00 8.564 4.001 1.942579703751 0.0574229 0.95917266540330 -0.3401305 178.4419 /L 2015-Dec-25 00:00 8.479 3.916 1.942619615925 0.0807888 0.95909800654613 0.0816224 179.6918 /L 2015-Dec-26 00:00 8.531 3.968 1.942673021590 0.1041497 0.95926696673316 0.5034760 179.0195 /T 2015-Dec-27 00:00 8.600 4.035 1.942739917445 0.1275043 0.95967955821171 0.9252657 177.7582 /T 2015-Dec-28 00:00 8.655 4.089 1.942820299366 0.1508510 0.96033568920636 1.3467939 176.4953 /T 2015-Dec-29 00:00 8.703 4.135 1.942914162403 0.1741886 0.96123514268329 1.7678241 175.2332 /T 2015-Dec-30 00:00 8.748 4.177 1.943021500782 0.1975155 0.96237755398790 2.1880826 173.9725 /T 2015-Dec-31 00:00 8.790 4.216 1.943142307908 0.2208303 0.96376239157112 2.6072667 172.7139 /T $$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. 'APmag S-brt' = The asteroids' approximate apparent airless visual magnitude and surface brightness using the standard IAU H-G system magnitude model: APmag = H + 5*log10(delta) + 5*log10(r) - 2.5*log10((1-G)*phi_1 + G*phi_2) For solar phase angles >90 deg, the error could exceed 1 magnitude. For phase angles >120 degrees, output values are rounded to the nearest integer to indicate error could be large and unknown. For Earth-based observers, the estimated dimming due to atmospheric absorption (extinction) is available as a separate, requestable quantity. Surface brightness is the average airless visual magnitude of a square-arcsecond of the illuminated portion of the apparent disk. It is computed only if the target radius is known. Units: MAGNITUDES & MAGNITUDES PER SQUARE ARCSECOND '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 'delta deldot' = Apparent range ("delta", light-time aberrated) and range-rate ("delta-dot") of the target center relative to the observer. A positive "deldot" means the target center is moving away from the observer, negative indicates movement toward the observer. Units: AU and KM/S 'S-O-T /r' = Sun-Observer-Target apparent SOLAR ELONGATION ANGLE seen from the observers' location at print-time. The '/r' column provides a code indicating the targets' apparent position relative to the Sun in the observers' sky, as described below: Case A: For an observing location on the surface of a rotating body, that body rotational sense is considered: /T indicates target TRAILS Sun (evening sky: rises and sets AFTER Sun) /L indicates target LEADS Sun (morning sky: rises and sets BEFORE Sun) Case B: For an observing point that does not have a rotational model (such as a spacecraft), the "leading" and "trailing" condition is defined by the observers' heliocentric ORBITAL motion: * If continuing in the observers' current direction of heliocentric motion would encounter the targets' apparent longitude first, followed by the Sun's, the target LEADS the Sun as seen by the observer. * If the Sun's apparent longitude would be encountered first, followed by the targets', the target TRAILS the Sun. Two other codes can be output: /* indicates observer is Sun-centered (undefined) /? Target is aligned with Sun center (no lead or trail) The S-O-T solar elongation angle is numerically the minimum separation angle of the Sun and target in the sky in any direction. It does NOT indicate the amount of separation in the leading or trailing directions, which would be defined along the equator of a spherical coordinate system. Units: DEGREES 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 ************************************************************************************************************** !$$SOF COMMAND = '27' START_TIME = '2015-12-01' STOP_TIME = '2015-12-31' STEP_SIZE = '1 day' QUANTITIES = '9,19,20,23'