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JPL Small-Body Database Browser
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(2018 SD3)
Classification: Apollo [NEO]          SPK-ID: 3831067
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2755804873253395 0.00022307  
a 1.379425945021726 0.00043118 au
q .9992830708634215 5.0991e-06 au
i 12.00607359446157 0.007127 deg
node 187.4295337120715 0.00010009 deg
peri 202.0096576341155 0.0043583 deg
M 114.2624133576706 0.050392 deg
tp 2458412.677808305536
(2018-Oct-21.17780831)
0.0053467 TDB
period 591.7605538257945
1.62
0.27746
0.0007596
d
yr
n .6083541690512521 0.00028524 deg/d
Q 1.75956881918003 0.00055001 au
  Orbit Determination Parameters
   # obs. used (total)      22  
   data-arc span      2 days  
   first obs. used      2018-09-30  
   last obs. used      2018-10-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .29925  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Oct-03 03:38:38  

Additional Information
 Earth MOID = .0131408 au 
 Jupiter MOID = 3.68955 au 
 T_jup = 4.740 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 27.9   .31488 E2018T36 autocmod 2.6n

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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