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(2013 GM3)
Classification: Aten [NEO]          SPK-ID: 3634154
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2867993948513905 0.00029372  
a .8355742080974912 6.8085e-05 au
q .5959320308617009 0.00019687 au
i .01351816639207765 0.0010477 deg
node 326.8791153434445 28.514 deg
peri 22.48818351310414 28.484 deg
M 352.3462074367575 0.14521 deg
tp 2459006.431303576935
(2020-Jun-05.93130358)
0.11326 TDB
period 278.9818603069107
0.76
0.034098
9.336e-05
d
yr
n 1.290406478772349 0.00015772 deg/d
Q 1.075216385333281 8.7612e-05 au
  Orbit Determination Parameters
   # obs. used (total)      61  
   data-arc span      12 days  
   first obs. used      2013-04-01  
   last obs. used      2013-04-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .79234  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:46:16  

Additional Information
 Earth MOID = 9.65353E-5 au 
 Jupiter MOID = 4.30064 au 
 T_jup = 6.995 
[ 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 MPO265055  

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