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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08063651529059586 6.4792e-08  
a 2.419744923883568 1.8272e-08 au
q 2.224625125329489 1.5998e-07 au
i 6.5805075028451 8.5194e-06 deg
node 201.5373965145406 5.545e-05 deg
peri 301.4679309701043 7.3449e-05 deg
M 126.8116204767387 4.8077e-05 deg
tp 2458516.205697749821
(2019-Feb-01.70569775)
0.00018284 TDB
period 1374.842054337166
3.76
1.5572e-05
4.263e-08
d
yr
n .2618482602160158 2.9659e-09 deg/d
Q 2.614864722437646 1.9745e-08 au
  Orbit Determination Parameters
   # obs. used (total)      228  
   data-arc span      8029 days (21.98 yr)  
   first obs. used      1997-05-05  
   last obs. used      2019-04-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56449  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 19:43:17  

Additional Information
 Earth MOID = 1.2443 au 
 Jupiter MOID = 2.39884 au 
 T_jup = 3.501 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.8   n/a MPO469981  

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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