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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 ]

[ hide orbit diagram ]

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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 40 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4703768428817504 3.3358e-08  
a .851239183990538 1.2551e-08 au
q .4508359840878314 3.2132e-08 au
i 2.95050827084543 3.3335e-06 deg
node 91.37606971549837 7.2133e-05 deg
peri 69.19031427229631 6.8715e-05 deg
M 285.9180746451664 2.1102e-05 deg
tp 2459259.531741711917
(2021-Feb-14.03174171)
1.8025e-05 TDB
period 286.863859362474
0.79
6.3447e-06
1.737e-08
d
yr
n 1.254950696124857 2.7756e-08 deg/d
Q 1.251642383893245 1.8455e-08 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] 1.20766323908902E-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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .43137  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 00:01:41  

Additional Information
 Earth MOID = .0236932 au 
 Jupiter MOID = 3.72977 au 
 T_jup = 6.826 
 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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