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(2014 AB17)
Classification: Apollo [NEO]          SPK-ID: 3655756
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 2456667.5 (2014-Jan-10.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .599200217761338 0.001372  
a 1.949364857002216 0.0058859 au
q .7813050101901886 0.0003154 au
i 5.683386013347715 0.0086806 deg
node 143.6595911361352 0.017821 deg
peri 33.63500512335256 0.013118 deg
M 343.4517069236826 0.084883 deg
tp 2456713.197119827871
(2014-Feb-24.69711983)
0.027433 TDB
period 994.1184303520034
2.72
4.5025
0.01233
d
yr
n .3621298921824928 0.0016401 deg/d
Q 3.117424703814244 0.0094127 au
  Orbit Determination Parameters
   # obs. used (total)      102  
   data-arc span      7 days  
   first obs. used      2014-01-05  
   last obs. used      2014-01-12  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .16801  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:13:47  

Additional Information
 Earth MOID = .0467912 au 
 Jupiter MOID = 1.85108 au 
 T_jup = 3.644 
[ 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 23.0   n/a E2014B08  

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