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(2014 GG49)
Classification: Apollo [NEO]          SPK-ID: 3667484
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 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4057073279629211 0.00055777  
a 1.401431176647309 0.00096442 au
q .8328602786457969 0.00020853 au
i 4.325005191857874 0.0050311 deg
node 35.3683420985201 9.1256e-05 deg
peri 239.9574237278423 0.0075561 deg
M 217.3671173251039 1.5029 deg
tp 2459240.589544543654
(2021-Jan-26.08954454)
2.7776 TDB
period 605.9769277237482
1.66
0.62552
0.001713
d
yr
n .5940820244630109 0.00061324 deg/d
Q 1.970002074648821 0.0013557 au
  Orbit Determination Parameters
   # obs. used (total)      44  
   data-arc span      10 days  
   first obs. used      2014-04-09  
   last obs. used      2014-04-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .45875  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:41:36  

Additional Information
 Earth MOID = .0076924 au 
 Jupiter MOID = 3.1695 au 
 T_jup = 4.659 
[ 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 25.7   n/a MPO294934  

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