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(2016 SG)
Classification: Apollo [NEO]          SPK-ID: 3759668
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.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5860044469730896 0.00050416  
a 1.746935700966731 0.0017883 au
q .723223611624175 0.00014039 au
i 5.854809301684812 0.0049158 deg
node .7704042025471117 0.0002048 deg
peri 79.42909856603384 0.0013231 deg
M 1.460324617922656 1.1018 deg
tp 2459393.078939826625
(2021-Jun-27.57893983)
2.5758 TDB
period 843.3615699549483
2.31
1.295
0.003546
d
yr
n .4268631780544979 0.00065545 deg/d
Q 2.770647790309286 0.0028362 au
  Orbit Determination Parameters
   # obs. used (total)      47  
   data-arc span      5 days  
   first obs. used      2016-09-22  
   last obs. used      2016-09-27  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .33356  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 17:42:55  

Additional Information
 Earth MOID = .00645301 au 
 Jupiter MOID = 2.54649 au 
 T_jup = 3.913 
[ 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 26.6   n/a E2016-TE1  

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