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(2013 UV3)
Classification: Apollo [NEO]          SPK-ID: 3653193
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5456991819958205 0.00046207  
a 1.26904537817004 0.00078597 au
q .5765283533870726 0.00022934 au
i 1.296217230265863 0.0019864 deg
node 212.9918118083024 0.0032064 deg
peri 284.3870096546722 0.0056804 deg
M 180.5769571582556 1.5314 deg
tp 2459260.749480552975
(2021-Feb-15.24948055)
2.463 TDB
period 522.1726903924368
1.43
0.4851
0.001328
d
yr
n .6894270930359139 0.00064048 deg/d
Q 1.961562402953008 0.0012149 au
  Orbit Determination Parameters
   # obs. used (total)      50  
   data-arc span      4 days  
   first obs. used      2013-10-25  
   last obs. used      2013-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .28023  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:44:01  

Additional Information
 Earth MOID = .00138065 au 
 Jupiter MOID = 3.08415 au 
 T_jup = 4.928 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456592.5 (2013-Oct-27.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5468676474759062 0.00046933  
q .5810736586021055 0.00023452 au
tp 2456650.063130127493
(2013-Dec-23.56313013)
0.02312 TDB
node 213.6059103356874 0.00030962 deg
peri 282.909719116656 0.00078437 deg
i 1.533583126098114 0.0015454 deg
  Orbit Determination Parameters
   # obs. used (total)      50  
   data-arc span      4 days  
   first obs. used      2013-10-25  
   last obs. used      2013-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .28023  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:44:01  

Additional Information
 Jupiter MOID = 3.08415 au 
 T_jup = 4.928 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.202705839933082E-7 -1.100623347476726E-7 -1.08509587698129E-5 1.440078431632769E-7 3.43884559877171E-7 7.245479997639805E-7
q -1.100623347476726E-7 5.499851708510034E-8 5.421828509962369E-6 -7.196726206968464E-8 -1.723671901492066E-7 -3.619279989730779E-7
tp -1.08509587698129E-5 5.421828509962369E-6 .0005345405211101981 -7.093976799914913E-6 -1.693205511560882E-5 -3.569386619150961E-5
node 1.440078431632769E-7 -7.196726206968464E-8 -7.093976799914913E-6 9.586473944020441E-8 2.246678565233206E-7 4.744402427758141E-7
peri 3.43884559877171E-7 -1.723671901492066E-7 -1.693205511560882E-5 2.246678565233206E-7 6.152351280108468E-7 1.11547274287154E-6
i 7.245479997639805E-7 -3.619279989730779E-7 -3.569386619150961E-5 4.744402427758141E-7 1.11547274287154E-6 2.388185320486531E-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 26.8   n/a E2013U80  

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