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(2015 GZ5)
Classification: Apollo [NEO]          SPK-ID: 3715535
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4074105613829628 0.00058351  
a 1.456259865983379 0.0013485 au
q .8629642164636127 5.0643e-05 au
i 21.75548647057209 0.021967 deg
node 20.14635144524316 3.3988e-05 deg
peri 117.3794374917906 0.020761 deg
M .125801508633412 1.5148 deg
tp 2459000.275694410279
(2020-May-30.77569441)
2.7005 TDB
period 641.8842919829477
1.76
0.89158
0.002441
d
yr
n .5608487456327468 0.00077902 deg/d
Q 2.049555515503146 0.0018979 au
  Orbit Determination Parameters
   # obs. used (total)      34  
   data-arc span      6 days  
   first obs. used      2015-04-08  
   last obs. used      2015-04-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .53729  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-17 06:10:40  

Additional Information
 Earth MOID = .0164265 au 
 Jupiter MOID = 3.10688 au 
 T_jup = 4.471 
[ 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 25.3   n/a MPO477787  

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