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(2014 OF300)
Classification: Apollo [NEO]          SPK-ID: 3678251
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 2456868.5 (2014-Jul-30.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .614715919540203 0.0020497  
a 2.034925145742512 0.0096844 au
q .7840242635819221 0.00043982 au
i 4.735085854346901 0.012945 deg
node 311.726382160842 0.00065541 deg
peri 69.8770011195727 0.0048416 deg
M 342.0873292770506 0.14519 deg
tp 2456921.256858445950
(2014-Sep-20.75685845)
0.05101 TDB
period 1060.281257568651
2.90
7.569
0.02072
d
yr
n .3395325508493117 0.0024238 deg/d
Q 3.285826027903102 0.015638 au
  Orbit Determination Parameters
   # obs. used (total)      27  
   data-arc span      8 days  
   first obs. used      2014-07-29  
   last obs. used      2014-08-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .36009  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:28  

Additional Information
 Earth MOID = .005324 au 
 Jupiter MOID = 2.21389 au 
 T_jup = 3.540 
[ 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 26.3   n/a MPO302051  

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