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JPL Small-Body Database Browser
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(2010 TG19)
Classification: Apollo [NEO]          SPK-ID: 3548082
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .563361649055957 9.2177e-05  
a 2.108752366976979 0.0004303 au
q .9207621560661754 6.4961e-06 au
i 6.916621615772492 0.00082483 deg
node 208.3272042458669 6.1765e-05 deg
peri 216.9682706390305 0.0018332 deg
M 165.8872055378614 0.37787 deg
tp 2458881.096703459452
(2020-Feb-01.59670346)
1.0163 TDB
period 1118.50209395594
3.06
0.34235
0.0009373
d
yr
n .3218590308818688 9.8515e-05 deg/d
Q 3.296742577887782 0.00067271 au
  Orbit Determination Parameters
   # obs. used (total)      182  
   data-arc span      15 days  
   first obs. used      2010-10-07  
   last obs. used      2010-10-22  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .48604  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 04:15:16  

Additional Information
 Earth MOID = .00133511 au 
 Jupiter MOID = 2.07104 au 
 T_jup = 3.512 
[ 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 23.9   n/a MPO186370  
rotation period rot_per 0.0193935 h n/a LCDB (Rev. 2020-October); Warner et al., 2009 Published Reference List:
[Birtwhistle, P. (2011) Minor Planet Bull. 38, 104-106.]

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