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(2019 TZ6)
Classification: Apollo [NEO]          SPK-ID: 3879168
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .353098836331349 0.00022659  
a 1.008037145256997 0.00012555 au
q .6521004022879762 0.00015813 au
i 10.7858909762432 0.0082136 deg
node 17.33338186951813 0.00019784 deg
peri 110.0432142360748 0.008021 deg
M 157.8260748453851 0.012624 deg
tp 2458838.434906003708
(2019-Dec-20.93490600)		 0.019183 TDB
period 369.6691683919872
1.01		 0.06906
0.0001891		 d
yr
n .9738437250960181 0.00018193 deg/d
Q 1.363973888226017 0.00016988 au
   Orbit Determination Parameters
   # obs. used (total)      24  
   first obs. used      2019-10-10  
   last obs. used      2019-10-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .28742  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-11 07:12:07  

Additional Information
 Earth MOID = .00278427 au 
 Jupiter MOID = 3.7076 au 
 T_jup = 5.971 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458766.5 (2019-Oct-10.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3520308661786198 0.00022897  
q .6574787341437736 0.00016586 au
tp 2458838.113376476722
(2019-Dec-20.61337648)		 0.018373 TDB
node 17.36445144355494 0.00014895 deg
peri 108.9393334715465 0.0073423 deg
i 10.92438809294149 0.008001 deg
   Orbit Determination Parameters
   # obs. used (total)      24  
   first obs. used      2019-10-10  
   last obs. used      2019-10-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .28742  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-11 07:12:07  

Additional Information
 Jupiter MOID = 3.7076 au 
 T_jup = 5.971 
Orbit Covariance (6×6)
  e q tp node peri i
e 5.242592728110929E-8 -3.724589517078833E-8 -4.160504343392071E-6 3.121336999736949E-8 -9.225057740689434E-8 1.811952794979432E-6
q -3.724589517078833E-8 2.750988051102286E-8 2.867690533635974E-6 -2.024649662857615E-8 -1.718628931365362E-7 -1.24926101408027E-6
tp -4.160504343392071E-6 2.867690533635974E-6 .0003375835810827176 -2.639119303032094E-6 2.727385228381337E-5 -.000146992216162129
node 3.121336999736949E-8 -2.024649662857615E-8 -2.639119303032094E-6 2.218679828435001E-8 -4.915983452214225E-7 1.14864928148258E-6
peri -9.225057740689434E-8 -1.718628931365362E-7 2.727385228381337E-5 -4.915983452214225E-7 5.390964841455775E-5 -1.179907690411514E-5
i 1.811952794979432E-6 -1.24926101408027E-6 -.000146992216162129 1.14864928148258E-6 -1.179907690411514E-5 6.40154026810284E-5

[ 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 27.7   .27283 MPO502096 autocmod 2.8

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