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JPL Small-Body Database Browser
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(2016 CW193)
Classification: Apollo [NEO, PHA]          SPK-ID: 3743606
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 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6706039885817739 3.3857e-08  
a 2.47870333115741 3.5527e-08 au
q .8164749907723211 9.2391e-08 au
i 6.507706404040398 1.1551e-05 deg
node 184.9368153388362 7.7404e-05 deg
peri 235.3084520892014 7.4981e-05 deg
M 310.3290689729839 6.829e-06 deg
tp 2458797.168611750848
(2019-Nov-09.66861175)
3.0939e-05 TDB
period 1425.39507044466
3.90
3.0645e-05
8.39e-08
d
yr
n .2525615581704628 5.4299e-09 deg/d
Q 4.140931671542499 5.9351e-08 au
  Orbit Determination Parameters
   # obs. used (total)      93  
   data-arc span      1344 days (3.68 yr)  
   first obs. used      2016-01-22  
   last obs. used      2019-09-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57882  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-29 13:42:02  

Additional Information
 Earth MOID = .00421529 au 
 Jupiter MOID = 1.28533 au 
 T_jup = 3.117 
[ 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 21.7   n/a MPO373618  

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