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(2019 TZ)
Classification: Apollo [NEO]          SPK-ID: 3873326
[ 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 2458759.5 (2019-Oct-03.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3842427662814318 0.0012121  
a 1.087389639953475 0.00095584 au
q .6695680366719818 0.00072961 au
i 1.240616040612554 0.0053935 deg
node 150.3685135454407 0.055516 deg
peri 326.6808995580571 0.057504 deg
M 298.2636124526706 0.15217 deg
tp 2458830.525602434627
(2019-Dec-13.02560243)		 0.08142 TDB
period 414.167687684405
1.13		 0.5461
0.001495		 d
yr
n .869213148936716 0.0011461 deg/d
Q 1.505211243234969 0.0013231 au
   Orbit Determination Parameters
   # obs. used (total)      17  
   data-arc span      4 days  
   first obs. used      2019-10-02  
   last obs. used      2019-10-06  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .43709  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 21:55:23  

Additional Information
 Earth MOID = .0155036 au 
 Jupiter MOID = 3.59204 au 
 T_jup = 5.629 
[ 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 26.6   .38294 MPO492740 autocmod 2.8

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