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(2016 FZ12)
Classification: Apollo [NEO]          SPK-ID: 3748477
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2986915592598468 0.00042315  
a 1.129350168229985 0.00036182 au
q .7920228055310008 0.00022515 au
i 1.751491460256451 0.0024631 deg
node 348.5166414085256 0.015303 deg
peri 106.6701965120548 0.015424 deg
M 230.7762055295425 0.64959 deg
tp 2459157.855289663370
(2020-Nov-04.35528966)
0.86662 TDB
period 438.3705378018726
1.20
0.21066
0.0005768
d
yr
n .821223072620603 0.00039465 deg/d
Q 1.46667753092897 0.00046989 au
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      4 days  
   first obs. used      2016-03-28  
   last obs. used      2016-04-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .27094  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:27:10  

Additional Information
 Earth MOID = .00544273 au 
 Jupiter MOID = 3.69772 au 
 T_jup = 5.496 
[ 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 26.7   n/a E2016G28  

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