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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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .662452336454921 0.0012164  
a 1.895253860521628 0.0056504 au
q .6397385124438666 0.00039819 au
i 8.789567784604131 0.015335 deg
node 204.9867016213026 0.0020411 deg
peri 262.1375160571256 0.00047699 deg
M 339.1531879905791 0.10773 deg
tp 2458821.686984104186
(2019-Dec-04.18698410)
0.038384 TDB
period 953.0145073754526
2.61
4.2619
0.01167
d
yr
n .3777487091895583 0.0016893 deg/d
Q 3.150769208599389 0.0093935 au
  Orbit Determination Parameters
   # obs. used (total)      41  
   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      .47615  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-04 07:20:13  

Additional Information
 Earth MOID = .00532144 au 
 Jupiter MOID = 2.11461 au 
 T_jup = 3.639 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 1.479727127699159E-6 -4.843696458558827E-7 -4.669139859754065E-5 -2.482694862104864E-6 5.404486217077219E-7 1.865438237833995E-5
q -4.843696458558827E-7 1.585539826412183E-7 1.528375700615532E-5 8.126510840676376E-7 -1.771416440739602E-7 -6.106274650904837E-6
tp -4.669139859754065E-5 1.528375700615532E-5 .001473306084761382 7.834022495244771E-5 -1.704412015030794E-5 -.0005886214079119303
node -2.482694862104864E-6 8.126510840676376E-7 7.834022495244771E-5 4.166094673785873E-6 -9.034563800151666E-7 -3.129859459342418E-5
peri 5.404486217077219E-7 -1.771416440739602E-7 -1.704412015030794E-5 -9.034563800151666E-7 2.275235047912908E-7 6.813754467027917E-6
i 1.865438237833995E-5 -6.106274650904837E-6 -.0005886214079119303 -3.129859459342418E-5 6.813754467027917E-6 .0002351693622018918

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 5 autocmod 2.8

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