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(2014 OM207)
Classification: Apollo [NEO]          SPK-ID: 3676117
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 2456867.5 (2014-Jul-29.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5840460340394195 0.00090232  
a 2.430625447289602 0.0052568 au
q 1.01102829456482 6.5971e-06 au
i 2.24848630143055 0.0023696 deg
node 122.7782255958449 0.00012991 deg
peri 168.627587568712 0.0020386 deg
M 3.244496818736896 0.010788 deg
tp 2456855.025580654729
(2014-Jul-16.52558065)
0.0010123 TDB
period 1384.125556346162
3.79
4.4903
0.01229
d
yr
n .2600920114142925 0.00084377 deg/d
Q 3.850222600014384 0.0083271 au
  Orbit Determination Parameters
   # obs. used (total)      8  
   data-arc span      5 days  
   first obs. used      2014-07-26  
   last obs. used      2014-07-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .47175  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:30  

Additional Information
 Earth MOID = .00124024 au 
 Jupiter MOID = 1.36418 au 
 T_jup = 3.249 
[ 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 29.1   n/a MPO302048  

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