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(2013 GJ69)
Classification: Amor [NEO]          SPK-ID: 3634713
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5412071213081147 4.0958e-06  
a 2.218228985658933 1.9113e-05 au
q 1.017707661928243 3.91e-07 au
i 6.625064908514006 6.9759e-05 deg
node 201.6738484706281 3.1591e-05 deg
peri 11.09131417616798 0.0005952 deg
M 113.8401322773887 0.010892 deg
tp 2458818.906576167575
(2019-Dec-01.40657617)		 0.031577 TDB
period 1206.724112415308
3.30		 0.015597
4.27e-05		 d
yr
n .2983283389269858 3.8558e-06 deg/d
Q 3.418750309389623 2.9458e-05 au
   Orbit Determination Parameters
   # obs. used (total)      23  
   # delay obs. used      2  
   # Doppler obs. used      1  
   data-arc span      6 days  
   first obs. used      2013-04-12  
   last obs. used      2013-04-18  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      4  
   norm. resid. RMS      .27042  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:58:03  

Additional Information
 Earth MOID = .0179422 au 
 Jupiter MOID = 1.54765 au 
 T_jup = 3.436 
[ 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 26.5   n/a MPO265059  

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