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(2011 FT29)
Classification: Apollo [NEO]          SPK-ID: 3560818
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.


Orbital Elements at Epoch 2455652.5 (2011-Apr-01.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6442479222767608 0.0022797  
a 1.754723704388761 0.0088666 au
q .6242466036665207 0.00084601 au
i .6852766411931481 0.0017526 deg
node 260.0672962553264 0.10475 deg
peri 23.63437240068972 0.10177 deg
M 336.7962255864715 0.20922 deg
tp 2455707.222719905763
(2011-May-25.72271991)
0.078653 TDB
period 849.0075284729929
2.32
6.435
0.01762
d
yr
n .4240245085311415 0.0032139 deg/d
Q 2.885200805111001 0.014579 au
  Orbit Determination Parameters
   # obs. used (total)      16  
   data-arc span      5 days  
   first obs. used      2011-03-31  
   last obs. used      2011-04-05  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .58711  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 04:56:17  

Additional Information
 Earth MOID = .0107687 au 
 Jupiter MOID = 2.29512 au 
 T_jup = 3.854 
[ show covariance matrix ]

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 25.2   n/a MPO196459  

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