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JPL Small-Body Database Browser
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(2019 TV)
Classification: Apollo [NEO]          SPK-ID: 3873322
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 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5000518537477856 0.0003888  
a 1.925221354432103 0.0014854 au
q .9625108472735071 3.2183e-05 au
i 6.6890561679246 0.0037132 deg
node 11.33523302109285 0.0003 deg
peri 30.69282360350005 0.010802 deg
M 291.5209216727606 0.081741 deg
tp 2458786.098660648675
(2019-Oct-29.59866065)
0.0097033 TDB
period 975.707025644142
2.67
1.1292
0.003092
d
yr
n .3689632138933665 0.00042702 deg/d
Q 2.887931861590698 0.0022282 au
  Orbit Determination Parameters
   # obs. used (total)      23  
   data-arc span      1 day  
   first obs. used      2019-10-03  
   last obs. used      2019-10-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .59467  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-20 06:05:35  

Additional Information
 Earth MOID = .00556621 au 
 Jupiter MOID = 2.55367 au 
 T_jup = 3.749 
[ 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 28.048   .48324 2 autocmod 2.8

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