Rise | Transit | Set Times Calculator
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General Data Query Portal
Built Around the NASA/JPL Horizons API
v1.00 - by Jay Tanner - 2025
NASA/JPL Body ID#, Record #, or Special Query or Command
INFO
Optional Location Name or Label
GPS Longitude +Pos = E
GPS Latitude +Pos = N
± Sea Level Altitude
meters
START:
Calendar Date
Time Zone
:
Daylight/Summer Time ?
STOP:
Calendar Date
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################################################################################ RISE | TRANSIT | SET TIMES CALCULATOR and General NASA/JPL Data Query Portal NASA/JPL BODY ID: 301 301 --------------- FOR OBSERVER AT Location Name or Label = Central New York State, USA GPS Longitude = -76.862737° +Positive = East GPS Latitude = +42.904788° Sea Level Altitude = +150 m Time Zone = UT-05:00 +Positive = East Start Date = 2025-Jan-04 Stop Date = 2025-Jan-04 Daylight/Summer Time = No ################################################################################ RISE / TRANSIT / SET TIMES TABLE NASA/JPL BODY ID: Moon (301) {source: DE441} Standard Time ============================================================================= Calen_Date Time Event Azim_Deg Dir Elev_Deg Vis_Mag Phase_Deg ============ ===== ======= ======== === ======== ======= ========= 2025-Jan-04 10:41 Rise 100.295 E - -8.883 59.9730 2025-Jan-04 16:24 Transit 180.013 S +40.344 -9.035 62.3507 2025-Jan-04 22:21 Set 264.354 W - -9.143 64.9162 ======================================== Phase_Deg General_Phase_Description =========== =========================== 0° New Moon 45 Waxing Crescent Moon 90 First Quarter Moon 135 Waxing Gibbous Moon 180 Full Moon 225 Waning Gibbous Moon 270 Last Quarter Moon 315 Waning Crescent Moon 360/0 New Moon ################################################################################
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API VERSION: 1.2 API SOURCE: NASA/JPL Horizons API ******************************************************************************* Revised: July 31, 2013 Moon / (Earth) 301 GEOPHYSICAL DATA (updated 2018-Aug-15): Vol. mean radius, km = 1737.53+-0.03 Mass, x10^22 kg = 7.349 Radius (gravity), km = 1738.0 Surface emissivity = 0.92 Radius (IAU), km = 1737.4 GM, km^3/s^2 = 4902.800066 Density, g/cm^3 = 3.3437 GM 1-sigma, km^3/s^2 = +-0.0001 V(1,0) = +0.21 Surface accel., m/s^2 = 1.62 Earth/Moon mass ratio = 81.3005690769 Farside crust. thick. = ~80 - 90 km Mean crustal density = 2.97+-.07 g/cm^3 Nearside crust. thick.= 58+-8 km Heat flow, Apollo 15 = 3.1+-.6 mW/m^2 Mean angular diameter = 31'05.2" Heat flow, Apollo 17 = 2.2+-.5 mW/m^2 Sid. rot. rate, rad/s = 0.0000026617 Geometric Albedo = 0.12 Mean solar day = 29.5306 d Obliquity to orbit = 6.67 deg Orbit period = 27.321582 d Semi-major axis, a = 384400 km Eccentricity = 0.05490 Mean motion, rad/s = 2.6616995x10^-6 Inclination = 5.145 deg Apsidal period = 3231.50 d Nodal period = 6798.38 d Perihelion Aphelion Mean Solar Constant (W/m^2) 1414+-7 1323+-7 1368+-7 Maximum Planetary IR (W/m^2) 1314 1226 1268 Minimum Planetary IR (W/m^2) 5.2 5.2 5.2 ******************************************************************************** ******************************************************************************* Ephemeris / API_USER Sat Jan 4 15:26:54 2025 Pasadena, USA / Horizons ******************************************************************************* Target body name: Moon (301) {source: DE441} Center body name: Earth (399) {source: DE441} Center-site name: (user defined site below) ******************************************************************************* Start time : A.D. 2025-Jan-04 00:00:00.0000 UT-05:00 Stop time : A.D. 2025-Jan-04 23:59:59.0000 UT-05:00 Step-size : 1 minutes ******************************************************************************* Target pole/equ : MOON_ME {East-longitude positive} Target radii : 1737.4, 1737.4, 1737.4 km {Equator_a, b, pole_c} Center geodetic : 283.137263, 42.904788, .150 {E-lon(deg),Lat(deg),Alt(km)} Center cylindric: 283.137263,4679.27044,4319.86216 {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 : Earth 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 Atmos refraction: YES (Earth refraction model) RA format : HMS Time format : CAL Calendar mode : Mixed Julian/Gregorian Time zone : UT-05:00 RTS-only print : TVH RTS elevation : 0. degrees EOP file : eop.250103.p250401 EOP coverage : DATA-BASED 1962-JAN-20 TO 2025-JAN-03. PREDICTS-> 2025-MAR-31 Units conversion: 1 au= 149597870.700 km, c= 299792.458 km/s, 1 day= 86400.0 s Table format : Comma Separated Values (spreadsheet) ****************************************************************************************** Date_(ZONE)_HR:MN, , ,Azimuth_(r-app), Elevation_(r-app), APmag, S-brt, S-O-T,/r ****************************************************************************************** $$SOE 2025-Jan-04 10:41,*,r, 100.295383187, -0.408183783, -8.883, 5.773, 59.9730,/T 2025-Jan-04 16:24,*,t, 180.012769955, 40.343729649, -9.035, 5.724, 62.3507,/T 2025-Jan-04 22:21, ,s, 264.354211310, -0.712902758, -9.143, 5.671, 64.9162,/T $$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: A time-zone correction has been requested. See header. NOTE: "n.a." in output means quantity "not available" at the print-time. SOLAR PRESENCE (OBSERVING SITE) Time tag is followed by a blank, then a solar-presence condition code: '*' Daylight (refracted solar upper-limb on or above apparent horizon) 'C' Civil twilight/dawn 'N' Nautical twilight/dawn 'A' Astronomical twilight/dawn ' ' Night OR geocentric ephemeris LUNAR PRESENCE WITH TARGET RISE/TRANSIT/SET EVENT MARKER (OBSERVING SITE) The solar-presence code column is immediately followed by another marker: 'm' Refracted upper-limb of Moon on or above apparent horizon ' ' Refracted upper-limb of Moon below apparent horizon OR geocentric The lunar presence marker (an ongoing state) can be over-ridden by a target event marker if an event has occurred since the last output step: 'r' Rise (target body on or went above cut-off RTS elevation) 'e' Elevation max (target body maximum elevation angle has occurred) 't' Transit (target body at or passed through observer meridian) 's' Set (target body on or went below cut-off RTS elevation) RTS MARKERS (TVH) Rise and set are with respect to the reference ellipsoid true visual horizon defined by the elevation cut-off angle. Horizon dip and yellow-light refraction (Earth only) are considered. Accuracy is < or = to twice the requested search step-size. 'Azimuth_(r-app), Elevation_(r-app),' = Refracted apparent azimuth and elevation of target center. Compensated for light-time, the gravitational deflection of light, stellar aberration approximate atmospheric yellow-light refraction, precession and nutation. Azimuth is measured clockwise from north: North(0) -> East(90) -> South(180) -> West(270) -> North (360) Elevation angle is with respect to a plane perpendicular to the reference surface local zenith direction. TOPOCENTRIC ONLY. Units: DEGREES 'APmag, S-brt,' = Moon's approximate apparent visual magnitude and surface brightness. When phase angle < 7 deg (within ~1 day of full Moon), computed magnitude tends to be about 0.12 too small. 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. Units: MAGNITUDES & MAGNITUDES PER SQUARE ARCSECOND '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 ******************************************************************************************
PHP Program by Jay Tanner - 2025
v1.00 - Revised: 1970-January-01-Thursday at Local Time 12:00:00 AM (UTC−05:00)