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JPL Small-Body Database Browser
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(2006 TU7)
Classification: Aten [NEO, PHA]          SPK-ID: 3350633
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 2456520.5 (2013-Aug-16.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4701239813633475 7.747e-08  
a .8507116387745115 2.7957e-09 au
q .4507716961617002 6.7022e-08 au
i 2.912387854146239 3.8256e-06 deg
node 91.88885411524352 0.00013701 deg
peri 68.63010703108559 0.00012984 deg
M 160.2165776236857 2.0135e-05 deg
tp 2456392.951035121112
(2013-Apr-10.45103512)
1.6393e-05 TDB
period 286.5972300584919
0.78
1.4128e-06
3.868e-09
d
yr
n 1.256118211353708 6.192e-09 deg/d
Q 1.250651581387323 4.11e-09 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] 1.68347151481873E-13 3.015E-14
ALN [SET] 1. n/a
NK [SET] 0. n/a
NM [SET] 2. n/a
R0 [SET] 1. n/a
  Orbit Determination Parameters
   # obs. used (total)      88  
   data-arc span      5511 days (15.09 yr)  
   first obs. used      2002-09-09  
   last obs. used      2017-10-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .42677  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jan-14 15:52:54  

Additional Information
 Earth MOID = .0228404 au 
 Jupiter MOID = 3.73338 au 
 T_jup = 6.829 
 Nongravitational accels. using nonstandard g(r) = (1 au/ r)^2 
[ 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 21.9   n/a MPO215114  

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