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(2013 AG69)
Classification: Apollo [NEO]          SPK-ID: 3623999
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 2456308.5 (2013-Jan-16.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5767374065851895 0.0012843  
a 1.467943631631404 0.0031816 au
q .6213256285110634 0.00053862 au
i 2.985034012953189 0.0071133 deg
node 293.8138544992934 0.00017755 deg
peri 86.24772862443314 0.0041272 deg
M 31.03382317877185 0.12839 deg
tp 2456252.499065244980
(2012-Nov-20.99906525)
0.049623 TDB
period 649.6246497143648
1.78
2.112
0.005782
d
yr
n .5541661637351498 0.0018017 deg/d
Q 2.314561634751745 0.0050166 au
  Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      5 days  
   first obs. used      2013-01-12  
   last obs. used      2013-01-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .48374  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-17 06:09:48  

Additional Information
 Earth MOID = .00302638 au 
 Jupiter MOID = 3.16068 au 
 T_jup = 4.411 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 1.649445820073268E-6 -6.917530904891007E-7 6.373141262072333E-5 2.241837443368459E-7 -5.293152781749645E-6 9.135081127759246E-6
q -6.917530904891007E-7 2.901117237465745E-7 -2.672793845400622E-5 -9.403011223849791E-8 2.22003662058359E-6 -3.831150406994067E-6
tp 6.373141262072333E-5 -2.672793845400622E-5 .002462473489539376 8.659159554284655E-6 -.0002044926044573966 .0003529533215773046
node 2.241837443368459E-7 -9.403011223849791E-8 8.659159554284655E-6 3.152269787290093E-8 -7.244278368643465E-7 1.243498164504036E-6
peri -5.293152781749645E-6 2.22003662058359E-6 -.0002044926044573966 -7.244278368643465E-7 1.70341652750995E-5 -2.932881878122108E-5
i 9.135081127759246E-6 -3.831150406994067E-6 .0003529533215773046 1.243498164504036E-6 -2.932881878122108E-5 5.059914824472304E-5

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 27.3   n/a MPO250177  

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