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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 39 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4702098950481787 3.3825e-08  
a .8507127373577953 4.323e-09 au
q .4506991904086376 2.9624e-08 au
i 2.920036122830218 3.4915e-06 deg
node 91.52354522990247 7.1345e-05 deg
peri 68.98936748348304 6.8103e-05 deg
M 34.97136995975163 1.541e-05 deg
tp 2458972.659118954625
(2020-May-03.15911895)
1.213e-05 TDB
period 286.597785213165
0.78
2.1846e-06
5.981e-09
d
yr
n 1.256115778188028 9.5747e-09 deg/d
Q 1.250726284306953 6.3557e-09 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] 1.206559080605465E-13 1.089E-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)      130  
   data-arc span      6551 days (17.94 yr)  
   first obs. used      2002-09-09  
   last obs. used      2020-08-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .43144  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Sep-22 06:42:09  

Additional Information
 Earth MOID = .0231336 au 
 Jupiter MOID = 3.73161 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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