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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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6442080404251501 0.0022771  
a 1.754583010750746 0.0088546 au
q .6242665276317477 0.00084502 au
i .6853228690515402 0.0017508 deg
node 260.0453406649613 0.10434 deg
peri 23.65547854960764 0.10137 deg
M 336.7929538119884 0.20899 deg
tp 2455707.223853616507
(2011-May-25.72385362)
0.078568 TDB
period 848.9054204631854
2.32
6.4261
0.01759
d
yr
n .4240755110311046 0.0032102 deg/d
Q 2.884899493869744 0.014559 au
  Orbit Determination Parameters
   # obs. used (total)      17  
   data-arc span      5 days  
   first obs. used      2011-03-31  
   last obs. used      2011-04-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .75109  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:53:56  

Additional Information
 Earth MOID = .0107675 au 
 Jupiter MOID = 2.29542 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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