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JPL Small-Body Database Browser
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(2016 VN3)
Classification: Apollo [NEO]          SPK-ID: 3763477
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 2457701.5 (2016-Nov-09.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6412165481762826 0.0010298  
a 1.999602402414374 0.0050565 au
q .7174242522132271 0.00024505 au
i 10.22783422517296 0.014624 deg
node 46.11207545999903 6.5926e-05 deg
peri 78.13888184525939 0.0029163 deg
M 343.0604456432975 0.073801 deg
tp 2457750.097438818694
(2016-Dec-27.59743882)
0.027391 TDB
period 1032.794464737944
2.83
3.9175
0.01073
d
yr
n .3485688704686703 0.0013222 deg/d
Q 3.281780552615521 0.0082988 au
  Orbit Determination Parameters
   # obs. used (total)      37  
   data-arc span      3 days  
   first obs. used      2016-11-08  
   last obs. used      2016-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .56519  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:22:19  

Additional Information
 Earth MOID = .0156186 au 
 Jupiter MOID = 1.94412 au 
 T_jup = 3.538 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 1.06049738281911E-6 -2.523224870023572E-7 -2.820693233185133E-5 6.600887985646513E-8 -2.960693616440421E-6 1.505710720982753E-5
q -2.523224870023572E-7 6.004752415667481E-8 6.710823044260949E-6 -1.567027579948908E-8 7.026850039175262E-7 -3.581601522488059E-6
tp -2.820693233185133E-5 6.710823044260949E-6 .0007502572599184978 -1.756672089217366E-6 7.880455716342427E-5 -.0004005109604128816
node 6.600887985646513E-8 -1.567027579948908E-8 -1.756672089217366E-6 4.346293079651192E-9 -1.890655915746838E-7 9.410442749101909E-7
peri -2.960693616440421E-6 7.026850039175262E-7 7.880455716342427E-5 -1.890655915746838E-7 8.504791092950103E-6 -4.215742138826394E-5
i 1.505710720982753E-5 -3.581601522488059E-6 -.0004005109604128816 9.410442749101909E-7 -4.215742138826394E-5 .0002138759266582938

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 26.2   n/a MPO389567  

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