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226470 (2003 SV168)
Classification: Main-belt Asteroid          SPK-ID: 2226470
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06641352537751744 7.3759e-08  
a 3.161492579191596 3.7968e-08 au
q 2.951526711552622 2.4383e-07 au
i 8.506731550490176 8.2918e-06 deg
node 346.4421306184904 3.38e-05 deg
peri 336.0939112541481 5.4187e-05 deg
M 27.03245845754478 4.0642e-05 deg
tp 2458846.322953976874
(2019-Dec-28.82295398)
0.00023206 TDB
period 2053.225630791061
5.62
3.6988e-05
1.013e-07
d
yr
n .175333872031054 3.1585e-09 deg/d
Q 3.37145844683057 4.049e-08 au
  Orbit Determination Parameters
   # obs. used (total)      358  
   data-arc span      6232 days (17.06 yr)  
   first obs. used      2003-08-30  
   last obs. used      2020-09-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57972  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-22 22:17:07  

Additional Information
 Earth MOID = 1.94206 au 
 Jupiter MOID = 1.95439 au 
 T_jup = 3.184 
[ 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 15.1   n/a MPO418209  

226470 (2003 SV168)          Discovered 2003-Sep-23 by NEAT at Haleakala
Reference: 20091202/Numbers.arcLast Updated: 2009-12-04

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