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JPL Small-Body Database Browser
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(2019 OM3)
Classification: Apollo [NEO]          SPK-ID: 3843408
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3628896554990463 0.00077065  
a 1.082868622346917 0.00068059 au
q .6899068010327172 0.00040098 au
i 12.70305675018358 0.030591 deg
node 306.2436986430571 0.00032538 deg
peri 256.25202738806 0.022959 deg
M 339.2993189564585 0.036185 deg
tp 2458624.167054686826
(2019-May-20.66705469)
0.063681 TDB
period 411.5874095802115
1.13
0.38803
0.001062
d
yr
n .8746623235321342 0.0008246 deg/d
Q 1.475830443661116 0.00092757 au
  Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      2 days  
   first obs. used      2019-07-30  
   last obs. used      2019-08-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .37181  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Aug-02 07:00:21  

Additional Information
 Earth MOID = .00655686 au 
 Jupiter MOID = 3.5394 au 
 T_jup = 5.635 
[ 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 26.557   .31089 2 autocmod 2.6q

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