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(2016 FY12)
Classification: Apollo [NEO]          SPK-ID: 3748476
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5922876211727772 0.00050112  
a 2.193999651193112 0.0025293 au
q .8945208169340405 6.8239e-05 au
i 6.310859074428706 0.0037627 deg
node 207.5494837963875 0.00046132 deg
peri 47.43107006522531 0.00066605 deg
M 146.3952732219105 0.87774 deg
tp 2458717.799429689274
(2019-Aug-22.29942969)
2.0594 TDB
period 1187.006940097389
3.25
2.0526
0.00562
d
yr
n .3032838207082963 0.00052444 deg/d
Q 3.493478485452183 0.0040273 au
  Orbit Determination Parameters
   # obs. used (total)      36  
   data-arc span      18 days  
   first obs. used      2016-03-29  
   last obs. used      2016-04-16  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .40345  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 16:46:50  

Additional Information
 Earth MOID = .00377434 au 
 Jupiter MOID = 1.60365 au 
 T_jup = 3.412 
[ 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 26.0   n/a MPO438023  

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