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(2016 GE135)
Classification: Apollo [NEO]          SPK-ID: 3750672
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3315318667546887 0.00050897  
a 1.401604367413949 0.00099794 au
q .9369278550336777 4.7956e-05 au
i 13.99250991721 0.025032 deg
node 21.56633588879643 0.0043357 deg
peri 78.19764258243003 0.0096772 deg
M 238.4861666597528 1.0222 deg
tp 2459205.078415602886
(2020-Dec-21.57841560)
1.9395 TDB
period 606.0892623708014
1.66
0.6473
0.001772
d
yr
n .593971915278305 0.00063436 deg/d
Q 1.86628087979422 0.0013288 au
  Orbit Determination Parameters
   # obs. used (total)      39  
   data-arc span      16 days  
   first obs. used      2016-03-30  
   last obs. used      2016-04-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .37261  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:26:41  

Additional Information
 Earth MOID = .110349 au 
 Jupiter MOID = 3.3749 au 
 T_jup = 4.663 
[ 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 22.9   n/a MPO374806  

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