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JPL Small-Body Database Browser
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C/2013 V3 (Nevski)
Classification: Halley-type Comet*          SPK-ID: 1003286
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 2456629.5 (2013-Dec-03.0) TDB
Reference: JPL 31 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .8909685922028165 1.1646e-05  
a 12.71828653247425 0.0013906 au
q 1.386692685403626 3.825e-06 au
i 32.13447939562106 0.00014419 deg
node 100.9181160202745 0.00013591 deg
peri 339.6433006262093 0.00014563 deg
M .7408688627761659 0.00012446 deg
tp 2456595.405825758412
(2013-Oct-29.90582576)
0.00015305 TDB
period 16566.90319117908
45.36
2.7172
0.007439
d
yr
n .02173007205062194 3.564e-06 deg/d
Q 24.04988037954487 0.0026296 au
  Orbit Determination Parameters
   # obs. used (total)      905  
   data-arc span      122 days  
   first obs. used      2013-11-06  
   last obs. used      2014-03-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-BIG16  
   condition code      4  
   norm. resid. RMS      .71148  
   source      ORB  
   producer      Otto Matic  
   solution date      2014-Jun-13 19:45:15  

Additional Information
 Earth MOID = .427244 au 
 T_jup = 1.611 
[ 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
comet total magnitude M1 15.2   1. 31 2 parameter fit from 191 observations, autocmod 2.5c
comet total magnitude slope K1 7.   n/a 31 autocmod 2.5c

[ show close-approach data ]
Alternate Designations
 Perihelion 
Year
(est.)
 New-Style 
Desig
Roman
 Numeral 
Year/
 Letter 
 2013.8   C/2013 V3       
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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