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(2016 TM10)
Classification: Apollo [NEO]          SPK-ID: 3760441
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 2457666.5 (2016-Oct-05.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6973545947867901 0.0015881  
a 2.112860526247181 0.0096879 au
q .639447530125074 0.00042355 au
i 13.59215304041078 0.029459 deg
node 10.31316295992914 0.0012518 deg
peri 86.24113282452655 0.0081384 deg
M 344.5175082107515 0.12213 deg
tp 2457714.743968876598
(2016-Nov-22.24396888)
0.04875 TDB
period 1121.772194811432
3.07
7.7153
0.02112
d
yr
n .3209207730991367 0.0022072 deg/d
Q 3.586273522369288 0.016444 au
  Orbit Determination Parameters
   # obs. used (total)      35  
   data-arc span      2 days  
   first obs. used      2016-10-04  
   last obs. used      2016-10-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .46636  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:23:21  

Additional Information
 Earth MOID = .0127493 au 
 Jupiter MOID = 1.92978 au 
 T_jup = 3.351 
[ 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 26.3   n/a MPO389508  

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