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(2016 TP2)
Classification: Apollo [NEO]          SPK-ID: 3760339
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4916735409286744 0.00026467  
a 1.467721121154574 0.00061386 au
q .7460814804207009 7.6429e-05 au
i 12.7096843344871 0.0063334 deg
node 192.4506994336811 0.00028187 deg
peri 258.0911915976858 0.0023595 deg
M 350.0030677056318 0.4402 deg
tp 2459018.535491945093
(2020-Jun-18.03549195)
0.80548 TDB
period 649.4769504332057
1.78
0.40746
0.001116
d
yr
n .5542921881367422 0.00034774 deg/d
Q 2.189360761888448 0.00091568 au
  Orbit Determination Parameters
   # obs. used (total)      75  
   data-arc span      3 days  
   first obs. used      2016-10-04  
   last obs. used      2016-10-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .37016  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:23:26  

Additional Information
 Earth MOID = .00517122 au 
 Jupiter MOID = 3.12721 au 
 T_jup = 4.447 
[ 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 26.6   n/a E2016-TE1  

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