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(2016 GC134)
Classification: Apollo [NEO]          SPK-ID: 3749345
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1559764648722878 0.00029855  
a 1.166220530863455 0.00037084 au
q .9843175751978902 3.5181e-05 au
i 4.770948340937459 0.0074275 deg
node 195.3128499585289 0.0020696 deg
peri 49.1568883975557 0.00094009 deg
M 227.7016551440991 0.62183 deg
tp 2459369.552407932494
(2021-Jun-04.05240793)
0.87522 TDB
period 460.0123071984394
1.26
0.21941
0.0006007
d
yr
n .7825877576894996 0.00037328 deg/d
Q 1.348123486529019 0.00042868 au
  Orbit Determination Parameters
   # obs. used (total)      24  
   data-arc span      14 days  
   first obs. used      2016-04-03  
   last obs. used      2016-04-17  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .63012  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 16:56:23  

Additional Information
 Earth MOID = .018075 au 
 Jupiter MOID = 3.65032 au 
 T_jup = 5.394 
[ 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 26.2   n/a MPO374803  

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