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JPL Small-Body Database Browser
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193457 (2000 XJ2)
Classification: Main-belt Asteroid          SPK-ID: 2193457
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09261876433969005 5.8769e-08  
a 2.566064501588512 2.0286e-08 au
q 2.328398778235441 1.5273e-07 au
i 1.048732402464308 5.4987e-06 deg
node 122.3438759584824 0.00046975 deg
peri 160.1159391378418 0.00047279 deg
M 322.8325830583575 5.7129e-05 deg
tp 2458755.509979502362
(2019-Sep-29.00997950)
0.00023844 TDB
period 1501.411645271686
4.11
1.7804e-05
4.874e-08
d
yr
n .2397743491158661 2.8432e-09 deg/d
Q 2.803730224941583 2.2164e-08 au
  Orbit Determination Parameters
   # obs. used (total)      258  
   data-arc span      8618 days (23.59 yr)  
   first obs. used      1995-09-26  
   last obs. used      2019-05-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .47302  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 13:12:29  

Additional Information
 Earth MOID = 1.31138 au 
 Jupiter MOID = 2.29606 au 
 T_jup = 3.426 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 17.0   n/a MPO436956  

193457 (2000 XJ2)          Discovered 2000-Dec-01 by Bohyunsan at Bohyunsan
Reference: 20081113/Numbers.arcLast Updated: 2008-11-17

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Alternate Designations
 2000 XJ2 = 1995 TF9 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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