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JPL Small-Body Database Browser
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183909 (2004 CW96)
Classification: Main-belt Asteroid          SPK-ID: 2183909
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

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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 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08067532349686089 6.4649e-08  
a 2.418174328185887 1.8893e-08 au
q 2.223087331987687 1.5979e-07 au
i 6.583168745529919 8.5528e-06 deg
node 201.5689504903088 5.6273e-05 deg
peri 300.9272447683464 7.455e-05 deg
M 22.52036604764077 4.8678e-05 deg
tp 2458514.578315888631
(2019-Jan-31.07831589)		 0.00018558 TDB
period 1373.503708361498
3.76		 1.6096e-05
4.407e-08		 d
yr
n .262103405916142 3.0716e-09 deg/d
Q 2.613261324384088 2.0417e-08 au
   Orbit Determination Parameters
   # obs. used (total)      220  
   data-arc span      8001 days (21.91 yr)  
   first obs. used      1997-05-05  
   last obs. used      2019-04-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56596  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 19:14:31  

Additional Information
 Earth MOID = 1.24345 au 
 Jupiter MOID = 2.40293 au 
 T_jup = 3.502 
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[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.7   n/a MPO433204  

183909 (2004 CW96)          Discovered 2004-Feb-12 by NEAT at Palomar
Reference: 20080420/Numbers.arcLast Updated: 2008-04-23

Alternate Designations
 2004 CW96 = 1997 JC7 = 2002 TW151 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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