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(2016 JZ5)
Classification: Apollo [NEO]          SPK-ID: 3752779
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 .3794783133486858 0.00019754  
a 1.555283701538275 0.00047162 au
q .9650872656998299 1.4603e-05 au
i 6.866883218658827 0.0028898 deg
node 219.9254430874863 0.0009153 deg
peri 328.5600603656447 0.0021602 deg
M 51.14101628935303 0.36007 deg
tp 2458899.857895036264
(2020-Feb-20.35789504)
0.66282 TDB
period 708.455959927564
1.94
0.32225
0.0008823
d
yr
n .5081473237049317 0.00023114 deg/d
Q 2.145480137376721 0.00065059 au
  Orbit Determination Parameters
   # obs. used (total)      63  
   data-arc span      9 days  
   first obs. used      2016-05-04  
   last obs. used      2016-05-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .52203  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:26:08  

Additional Information
 Earth MOID = .00118253 au 
 Jupiter MOID = 2.82272 au 
 T_jup = 4.350 
[ 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 27.0   n/a MPO378518  

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