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JPL Small-Body Database Browser
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(2019 TM)
Classification: Apollo [NEO]          SPK-ID: 3873207
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5957957062706301 0.00074138  
a 2.041139921334817 0.003377 au
q .8250375203059613 0.00014826 au
i 3.775687075940394 0.0042356 deg
node 1.068107562872314 0.0019155 deg
peri 69.60195679550991 0.0028456 deg
M 291.1701767540645 0.17532 deg
tp 2458804.148748588034
(2019-Nov-16.64874859)
0.013323 TDB
period 1065.142201945453
2.92
2.6434
0.007237
d
yr
n .3379830405202892 0.00083878 deg/d
Q 3.257242322363672 0.0053891 au
  Orbit Determination Parameters
   # obs. used (total)      42  
   data-arc span      13 days  
   first obs. used      2019-09-22  
   last obs. used      2019-10-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .39654  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-05 06:19:53  

Additional Information
 Earth MOID = .0131796 au 
 Jupiter MOID = 2.09026 au 
 T_jup = 3.553 
[ 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 24.875   .47214 3 autocmod 2.8

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