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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.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2986792280136237 0.00042236  
a 1.1292926198232 0.00035272 au
q .791996371932924 0.00023057 au
i 1.751336608417661 0.0024612 deg
node 348.5136649325117 0.015286 deg
peri 106.6790723548006 0.015493 deg
M 196.0338315196274 0.80376 deg
tp 2459596.145676365080
(2022-Jan-16.64567637)
1.0722 TDB
period 438.3370310932909
1.20
0.20536
0.0005622
d
yr
n .8212858473355438 0.00038478 deg/d
Q 1.466588867713476 0.00045807 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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .27162  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 16:46:50  

Additional Information
 Earth MOID = .00536496 au 
 Jupiter MOID = 3.69776 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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