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Ephemeris / API_USER Sun Oct 11 03:05:07 2026 Pasadena, USA      / Horizons
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Target body name: Voyager 2 (spacecraft) (-32)    {source: Voyager_2_ST+refit2022_m}
Center body name: Sun (10)                        {source: Voyager_2_ST+refit2022_m}
Center-site name: BODY CENTER
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Start time      : A.D. 2026-Oct-11 00:00:00.0000 UT 
Stop  time      : A.D. 2026-Oct-11 00:00:00.0000 UT 
Step-size       : DISCRETE TIME-LIST
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Center geodetic : 0.0, 0.0, 0.0                   {E-lon(deg),Lat(deg),Alt(km)}
Center cylindric: 0.0, 0.0, 0.0                   {E-lon(deg),Dxy(km),Dz(km)}
Center radii    : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
Output units    : KM-S
Calendar mode   : Gregorian
Output type     : GEOMETRIC cartesian states
Output format   : 2 (position and velocity)
EOP file        : eop.261009.p270105
EOP coverage    : DATA-BASED 1962-JAN-20 TO 2026-OCT-09. PREDICTS-> 2027-JAN-04
Reference frame : Ecliptic of J2000.0
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            JDUT ,            Calendar Date (UT ),                      X,                      Y,                      Z,                     VX,                     VY,                     VZ,
**************************************************************************************************************************************************************************************************
$$SOE
2461324.500000000, A.D. 2026-Oct-11 00:00:00.0000,  5.971131826045547E+09, -1.578531262229974E+10, -1.342920299429725E+10,  4.203400493911711E+00, -9.340270393900967E+00, -1.131663500898127E+01,
$$EOE
**************************************************************************************************************************************************************************************************
 
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" atomic 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 discontinuous civil UT time-scale 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,
a condition noted here as "UT~".

  Future but as yet undetermined leap-seconds can be expected to change
time-tags in the "UT~" interval and, in general, the UT scale may not be
suitable for purposes that assume time-tag continuity in the ephemeris.
Output in continuous TDB and TT timescales may instead be requested,
though these are not linked to Earth's rotation.

  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.
 
CALENDAR SYSTEM

  Calendar dates are given in the modern Gregorian system, extended prior to
its 1582-Oct-15 adoption. The Gregorian calendar more closely corresponds to
physical Earth seasons and orbital motion, but can differ by up to 10 days with
historical records made under the prior Julian calendar, more if the Julian
calendar was extended prior to its 45-Jan-1 BC adoption to label the historical
event. Select "mixed" calendar mode if correlation with historical dates prior
to A.D. 1582 is important.

REFERENCE FRAME AND COORDINATES

  Ecliptic at the standard reference epoch

    Reference epoch: J2000.0
    X-Y plane: adopted Earth orbital plane at the reference epoch
               Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
    X-axis   : ICRF
    Z-axis   : perpendicular to the X-Y plane in the directional (+ or -) sense
               of Earth's north pole at the reference epoch.

  Symbol meaning:

    JDUT     Julian Day Number, Universal Time
      X      X-component of position vector (km)
      Y      Y-component of position vector (km)
      Z      Z-component of position vector (km)
      VX     X-component of velocity vector (km/sec)                           
      VY     Y-component of velocity vector (km/sec)                           
      VZ     Z-component of velocity vector (km/sec)                           

ABERRATIONS AND CORRECTIONS

 Geometric state vectors have NO corrections or aberrations applied.

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/horizons_batch.txt
                  scripts        https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
    Inquiries   : Jon.D.Giorgini@jpl.nasa.gov
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