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JPL Small-Body Database Browser
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(2019 TP5)
Classification: Apollo [NEO]          SPK-ID: 3878621
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 2458766.5 (2019-Oct-10.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6624308397862341 0.0012242  
a 1.895154081962464 0.0056856 au
q .6397455719237596 0.00040075 au
i 8.789297161597428 0.015433 deg
node 204.9867370579217 0.0020539 deg
peri 262.1375055557754 0.00048121 deg
M 339.1512857346073 0.10841 deg
tp 2458821.687661429124
(2019-Dec-04.18766143)
0.038629 TDB
period 952.9392489906796
2.61
4.2883
0.01174
d
yr
n .3777785418968728 0.0017 deg/d
Q 3.150562592001168 0.0094519 au
  Orbit Determination Parameters
   # obs. used (total)      37  
   data-arc span      10 days  
   first obs. used      2019-10-07  
   last obs. used      2019-10-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .47238  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-18 06:01:49  

Additional Information
 Earth MOID = .00532127 au 
 Jupiter MOID = 2.11479 au 
 T_jup = 3.639 
[ 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 25.042   .63711 4 autocmod 2.8

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