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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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Orbit Diagram
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Note: This Java-based orbit viewer will eventually be retired.

Note: Make sure you have Java enabled on your browser to see the applet. This applet is provided as a 3D orbit visualization tool. The applet 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. For accurate long-term ephemerides, please instead use our Horizons system.

Note: If the applet is not working, here are some notes that might help.
Orbit Viewer

Additional Notes: the orbits shown in the applet are color coded. The planets are white lines, and the asteroid/comet is a blue line. The bright white line indicates the portion of the orbit that is above the ecliptic plane, and the darker portion is below the ecliptic plane. Likewise for the asteroid/comet orbit, the light blue indicates the portion above the ecliptic plane, and the dark blue the portion below the ecliptic plane.

Orbit Viewer applet originally written and kindly provided by Osamu Ajiki (AstroArts), and further modified by Ron Baalke (JPL).

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
0.038384 TDB
period 953.0145073754526
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 25.2   .63711 E2019X49 autocmod 2.8

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