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JPL Small-Body Database Browser
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(2014 VU6)
Classification: Amor [NEO]          SPK-ID: 3696013
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4029353278620695 4.2525e-06  
a 1.771187267361386 1.3652e-05 au
q 1.057513345082003 6.2104e-07 au
i 5.83530817707299 4.6888e-05 deg
node 211.0441090527044 4.6965e-05 deg
peri 239.2134707922046 5.4158e-05 deg
M 110.4504939395532 0.0096502 deg
tp 2458736.344102716881
(2019-Sep-09.84410272)
0.020026 TDB
period 860.9841353354806
2.36
0.0099547
2.725e-05
d
yr
n .4181261712327914 4.8344e-06 deg/d
Q 2.48486118964077 1.9153e-05 au
  Orbit Determination Parameters
   # obs. used (total)      44  
   data-arc span      100 days  
   first obs. used      2014-11-12  
   last obs. used      2015-02-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .42725  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:37:33  

Additional Information
 Earth MOID = .110364 au 
 Jupiter MOID = 2.7622 au 
 T_jup = 4.000 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457033.5 (2015-Jan-11.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4026223525613106 4.2052e-06  
q 1.058233686710228 7.5512e-07 au
tp 2457014.133414343494
(2014-Dec-22.63341434)
2.914e-05 TDB
node 211.0872479155438 4.6734e-05 deg
peri 239.1728979176875 5.4038e-05 deg
i 5.835136574097746 4.6865e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      44  
   data-arc span      100 days  
   first obs. used      2014-11-12  
   last obs. used      2015-02-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .42725  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:37:33  

Additional Information
 Jupiter MOID = 2.7622 au 
 T_jup = 4.000 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.768339821000655E-11 3.169177081301812E-12 -7.228142750908854E-11 -1.077551432996129E-10 2.844815903969009E-11 1.96314036767528E-10
q 3.169177081301812E-12 5.702086354242378E-13 -1.270567974998961E-11 -1.970419199863772E-11 5.714531683074023E-12 3.525422731703057E-11
tp -7.228142750908854E-11 -1.270567974998961E-11 8.491343361124004E-10 4.054355088515145E-13 8.55311839836127E-10 -8.22587836623926E-10
node -1.077551432996129E-10 -1.970419199863772E-11 4.054355088515145E-13 2.184110263734892E-9 -2.11690479049616E-9 -1.153554011775088E-9
peri 2.844815903969009E-11 5.714531683074023E-12 8.55311839836127E-10 -2.11690479049616E-9 2.920119872422185E-9 2.53089365970508E-10
i 1.96314036767528E-10 3.525422731703057E-11 -8.22587836623926E-10 -1.153554011775088E-9 2.53089365970508E-10 2.196365308735056E-9

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 23.5   n/a MPO331360  

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Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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