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(2012 VS76)
Classification: Aten [NEO]          SPK-ID: 3617713
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3862344267901189 0.00020581  
a .9909634535521464 5.8758e-05 au
q .6082192520994766 0.00016794 au
i .8058916627367044 0.0004256 deg
node 242.3156801859617 0.00059536 deg
peri 284.4430461096396 0.0039049 deg
M 1.339177766163502 0.26635 deg
tp 2459199.159642608669
(2020-Dec-15.65964261)
0.26647 TDB
period 360.3171088044784
0.99
0.032047
8.774e-05
d
yr
n .9991199174373634 8.8862e-05 deg/d
Q 1.373707655004816 8.1452e-05 au
  Orbit Determination Parameters
   # obs. used (total)      61  
   data-arc span      3 days  
   first obs. used      2012-11-13  
   last obs. used      2012-11-16  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .44472  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:13:25  

Additional Information
 Earth MOID = .00199187 au 
 Jupiter MOID = 3.59829 au 
 T_jup = 6.056 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456246.5 (2012-Nov-15.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .387020340844398 0.00020497  
q .6054179747962918 0.00015529 au
tp 2456316.056872217357
(2013-Jan-23.55687222)
0.015385 TDB
node 242.8724823318809 0.00073328 deg
peri 284.4082123173825 0.0022246 deg
i .7607399805876655 0.00046624 deg
  Orbit Determination Parameters
   # obs. used (total)      61  
   data-arc span      3 days  
   first obs. used      2012-11-13  
   last obs. used      2012-11-16  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .44472  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:13:25  

Additional Information
 Jupiter MOID = 3.59829 au 
 T_jup = 6.056 
Orbit Covariance (6×6)
  e q tp node peri i
e 4.201142271612855E-8 -3.182582315650704E-8 -3.153252103706134E-6 -8.286979879131326E-8 4.518731407644645E-7 9.517376152430843E-8
q -3.182582315650704E-8 2.411427476356203E-8 2.388383509155984E-6 6.163147135823487E-8 -3.422089958864135E-7 -7.202259470806447E-8
tp -3.153252103706134E-6 2.388383509155984E-6 .0002367033603599041 6.312662489693507E-6 -3.392531591778978E-5 -7.149626075103174E-6
node -8.286979879131326E-8 6.163147135823487E-8 6.312662489693507E-6 5.3769746145901E-7 -1.004699604045146E-6 -2.133919332873223E-7
peri 4.518731407644645E-7 -3.422089958864135E-7 -3.392531591778978E-5 -1.004699604045146E-6 4.948825522571574E-6 1.031960225462357E-6
i 9.517376152430843E-8 -7.202259470806447E-8 -7.149626075103174E-6 -2.133919332873223E-7 1.031960225462357E-6 2.173831805995883E-7

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 27.0   n/a MPO437985  

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