New Horizons Trajectory Options

[hal_9000]

I can not find NH's trajectory on ssd.jpl.nasa.gov and others..
Can anyone post it here?
Thanks!!

[hal_9000]

Some datas from ssd.jpl.nasa.gov
Revised: Jan 21, 2006 New Horizons Spacecraft -98
http://pluto.jhuapl.edu/index.php

Schedule:
2006-Jan-19... launch (Atlas V551 1st stage, Centaur 2nd, STAR 48B 3rd
2007-Feb ... Jupiter gravity assist
2015-Jul ... Pluto Charon encounter
2016+ ... Kuiper Belt object encounters

Mission Objectives:
* Map surface composition of Pluto and Charon
* Characterize geology and morphology of Pluto and Charon
* Characterize the neutral atmosphere of Pluto and its escape rate
* Search for an atmosphere around Charon
* Map surface temperatures on Pluto and Charon
* Search for rings and additional satellites around Pluto
* Conduct similar investigations of one or more Kuiper Belt Objects

Spacecraft:
1025 lbs (465 kg), 8 feet wide (2.5 m), RTG powered

Post-launch trajectory:
98_pred_20060119_20060125_od003 (released 2006-Jan-20)
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Ephemeris / PORT_LOGIN Sun Jan 22 05:05:04 2006 Pasadena, USA / Horizons
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Target body name: New Horizons Spacecraft (-98) {source: 98_pred_20060119_2006
Center body name: Sun (10) {source: DE405}
Center-site name: BODYCENTRIC
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Start time : A.D. 2006-Jan-20 00:00:00.0000 CT
Stop time : A.D. 2006-Jan-25 00:00:00.0000 CT
Step-size : 1440 minutes
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Center geodetic : 0.000000, 0.000000, 0.00000 {E-lon(deg),Lat(deg),Alt(km)}
Center cylindric: 0.00000, 0.000, 0.000 {E-lon(deg),Dxy(km),Dz(km)}
Center radii : 696000.0 x 696000.0 x 696000.0 k{Equator, meridian, pole}
System GM : 2.9591220828559093E-04 AU^3/d^2
Output units : AU-D, deg, Julian day number (Tp)
Output format : 10
Reference frame : ICRF/J2000.0
Output type : GEOMETRIC osculating elements
Coordinate systm: Ecliptic and Mean Equinox of Reference Epoch
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JDCT
OM W Tp
N MA TA
A AD PR
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$$SOE
2453755.500000000 = A.D. 2006-Jan-20 00:00:00.0000 (CT)
EC= 1.047218554066334E+00 QR= 9.840062365075131E-01 IN= 8.637488153620907E-01
OM= 1.197243484751520E+02 W = 3.598883622396694E+02 Tp= 2453755.386016075034
N = 1.036039523226175E-02 MA= 1.180918511812083E-03 TA= 1.646767917453556E-01
A =-2.083939790119697E+01 AD= 6.684586454211886E+91 PR= 1.157407291666667E+95
2453756.500000000 = A.D. 2006-Jan-21 00:00:00.0000 (CT)
EC= 1.034703732227682E+00 QR= 9.840055806051723E-01 IN= 8.604660258608851E-01
OM= 1.197223968639666E+02 W = 3.598809585157228E+02 Tp= 2453755.378474528436
N = 6.527877669034779E-03 MA= 7.321181081444460E-03 TA= 1.615135491083318E+00
A =-2.835445980707060E+01 AD= 6.684586454211886E+91 PR= 1.157407291666667E+95
2453757.500000000 = A.D. 2006-Jan-22 00:00:00.0000 (CT)
EC= 1.033619572849032E+00 QR= 9.840054836219194E-01 IN= 8.599730129954544E-01
OM= 1.197212053392239E+02 W = 3.598812906304760E+02 Tp= 2453755.377472462133
N = 6.224379773518880E-03 MA= 1.321141747506869E-02 TA= 3.054828040099436E+00
A =-2.926882765704868E+01 AD= 6.684586454211886E+91 PR= 1.157407291666667E+95
2453758.500000000 = A.D. 2006-Jan-23 00:00:00.0000 (CT)
EC= 1.033216622812397E+00 QR= 9.840054405674835E-01 IN= 8.597826670755985E-01
OM= 1.197203975997984E+02 W = 3.598816669695707E+02 Tp= 2453755.376919357106
N = 6.112811966113348E-03 MA= 1.909080472567998E-02 TA= 4.491903663153889E+00
A =-2.962388579130895E+01 AD= 6.684586454211886E+91 PR= 1.157407291666667E+95
2453759.500000000 = A.D. 2006-Jan-24 00:00:00.0000 (CT)
EC= 1.033006284284937E+00 QR= 9.840054265261474E-01 IN= 8.596827734047835E-01
OM= 1.197198120884730E+02 W = 3.598819761723426E+02 Tp= 2453755.376542187762
N = 6.054841621481327E-03 MA= 2.496688398525319E-02 TA= 5.925856385875568E+00
A =-2.981266894605479E+01 AD= 6.684586454211886E+91 PR= 1.157407291666667E+95
2453760.500000000 = A.D. 2006-Jan-25 00:00:00.0000 (CT)
EC= 1.032877115418984E+00 QR= 9.840054336563503E-01 IN= 8.596217217990696E-01
OM= 1.197193504998365E+02 W = 3.598822415259244E+02 Tp= 2453755.376259829383
N = 6.019333256683877E-03 MA= 3.084149960812402E-02 TA= 7.355907523452101E+00
A =-2.992979831461009E+01 AD= 6.684586454211886E+91 PR= 1.157407291666667E+95
$$EOE
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