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(2016 OA)
Classification: Apollo [NEO]          SPK-ID: 3755754
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 2457586.5 (2016-Jul-17.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6922243393687161 0.0015942  
a 2.445243402697046 0.011569 au
q .7525864036693719 0.00033772 au
i 1.085454615867138 0.0017226 deg
node 133.4662200996791 0.0094553 deg
peri 231.7526514402986 0.011544 deg
M 348.4516543495166 0.091577 deg
tp 2457631.302148790344
(2016-Aug-30.80214879)		 0.037336 TDB
period 1396.63065625757
3.82		 9.9113
0.02714		 d
yr
n .2577632091827777 0.0018292 deg/d
Q 4.13790040172472 0.019577 au
   Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      2 days  
   first obs. used      2016-07-16  
   last obs. used      2016-07-18  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .26298  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 17:20:57  

Additional Information
 Earth MOID = .0055267 au 
 Jupiter MOID = 1.31552 au 
 T_jup = 3.117 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 2.541436292332224E-6 -5.383042692478492E-7 -5.951814578267641E-5 1.423958009649517E-5 -1.73118331368439E-5 2.731775231451401E-6
q -5.383042692478492E-7 1.140579749367335E-7 1.260467583358543E-5 -2.999121385017687E-6 3.644193762495938E-6 -5.795829304447319E-7
tp -5.951814578267641E-5 1.260467583358543E-5 .001393955867800915 -.0003343099678641449 .0004065376456783322 -6.392851224445577E-5
node 1.423958009649517E-5 -2.999121385017687E-6 -.0003343099678641449 8.940204363510358E-5 -.0001090667570266338 1.476165301219686E-5
peri -1.73118331368439E-5 3.644193762495938E-6 .0004065376456783322 -.0001090667570266338 .0001332643719353179 -1.792497750140933E-5
i 2.731775231451401E-6 -5.795829304447319E-7 -6.392851224445577E-5 1.476165301219686E-5 -1.792497750140933E-5 2.967212553421233E-6

[ 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 25.4   n/a MPO384700  

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