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(2014 GD50)
Classification: Apollo [NEO]          SPK-ID: 3667491
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5226290331034792 1.0832e-06  
a 1.762811277773273 3.3327e-06 au
q .8415149241267187 3.3416e-07 au
i 35.01614563243444 5.0535e-05 deg
node 58.43980575620602 1.6583e-05 deg
peri 250.2670802745215 1.6406e-05 deg
M 187.5156555619227 0.0025638 deg
tp 2459410.094709950439
(2021-Jul-14.59470995)
0.0072497 TDB
period 854.8839378004814
2.34
0.0024243
6.637e-06
d
yr
n .4211097952386833 1.1942e-06 deg/d
Q 2.684107631419828 5.0745e-06 au
  Orbit Determination Parameters
   # obs. used (total)      79  
   data-arc span      232 days  
   first obs. used      2014-04-08  
   last obs. used      2014-11-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .44177  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Aug-10 06:18:09  

Additional Information
 Earth MOID = .0617334 au 
 Jupiter MOID = 3.10307 au 
 T_jup = 3.765 
[ 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 20.0   n/a MPO322309  

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