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JPL Small-Body Database Browser
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(2004 MO3)
Classification: Apollo [NEO]          SPK-ID: 3184470
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 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3357653694250928 1.3421e-07  
a 1.232335887479807 1.4109e-08 au
q .8185601729643501 1.7461e-07 au
i 2.553090410840245 8.3148e-06 deg
node 252.5972667407348 8.7702e-05 deg
peri 297.8922889773509 8.0341e-05 deg
M 351.2784536018485 7.5901e-05 deg
tp 2458612.605509298055
(2019-May-09.10550930)
0.00010555 TDB
period 499.6801195970814
1.37
8.581e-06
2.349e-08
d
yr
n .7204609226604555 1.2372e-08 deg/d
Q 1.646111601995264 1.8846e-08 au
  Orbit Determination Parameters
   # obs. used (total)      141  
   data-arc span      4082 days (11.18 yr)  
   first obs. used      2004-06-21  
   last obs. used      2015-08-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54791  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:12:35  

Additional Information
 Earth MOID = .0113999 au 
 Jupiter MOID = 3.31471 au 
 T_jup = 5.138 
[ 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 22.2   n/a MPO317263  

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