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(2013 VO11)
Classification: Apollo [NEO]          SPK-ID: 3653647
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3428808081927855 0.00046989  
a 1.197897641015921 0.00061198 au
q .7871615297321507 0.00016076 au
i 2.217394315544008 0.0028842 deg
node 52.25713546753696 0.012267 deg
peri 274.4491157065329 0.0097074 deg
M 194.3142771403114 1.4548 deg
tp 2459420.899486066931
(2021-Jul-25.39948607)
2.104 TDB
period 478.8814245104741
1.31
0.36697
0.001005
d
yr
n .7517518566689072 0.00057608 deg/d
Q 1.608633752299691 0.00082181 au
  Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      3 days  
   first obs. used      2013-11-09  
   last obs. used      2013-11-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .46994  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:43:45  

Additional Information
 Earth MOID = .00441562 au 
 Jupiter MOID = 3.72869 au 
 T_jup = 5.245 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456606.5 (2013-Nov-10.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3438193331410674 0.00047528  
q .7867182570565354 0.00021931 au
tp 2456547.476455993020
(2013-Sep-11.97645599)
0.020571 TDB
node 52.29200796401786 0.00034025 deg
peri 274.3312613318544 0.0020461 deg
i 2.215985753734151 0.0029722 deg
  Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      3 days  
   first obs. used      2013-11-09  
   last obs. used      2013-11-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .46994  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:43:45  

Additional Information
 Jupiter MOID = 3.72869 au 
 T_jup = 5.245 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.258905668886323E-7 -1.042305262937921E-7 9.776335885233834E-6 -8.489879522532429E-8 -9.354448457506364E-7 1.409135097432019E-6
q -1.042305262937921E-7 4.809849251154778E-8 -4.510534599327475E-6 3.907301483486572E-8 4.327027312183933E-7 -6.501290518220146E-7
tp 9.776335885233834E-6 -4.510534599327475E-6 .0004231663100481853 -3.667600624893672E-6 -4.038327165023326E-5 6.097955688514581E-5
node -8.489879522532429E-8 3.907301483486572E-8 -3.667600624893672E-6 1.157686739442335E-7 2.627320963311888E-7 -5.88178664723022E-7
peri -9.354448457506364E-7 4.327027312183933E-7 -4.038327165023326E-5 2.627320963311888E-7 4.186717853744819E-6 -5.774676863406285E-6
i 1.409135097432019E-6 -6.501290518220146E-7 6.097955688514581E-5 -5.88178664723022E-7 -5.774676863406285E-6 8.833716572643477E-6

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 28.3   n/a MPO275432  

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