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(2016 JB29)
Classification: Apollo [NEO]          SPK-ID: 3753295
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 42 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4949502688175568 6.7275e-06  
a 1.97133648430091 2.5755e-05 au
q .9956229614663175 2.5582e-07 au
i 6.278315983744682 5.8133e-05 deg
node 82.19866916942996 2.5755e-05 deg
peri 199.108439861945 1.098e-05 deg
M 150.9260149247055 0.0099458 deg
tp 2458576.660751825866
(2019-Apr-03.16075183)
0.019624 TDB
period 1010.973021574903
2.77
0.019812
5.424e-05
d
yr
n .3560925883454227 6.9783e-06 deg/d
Q 2.947050007135503 3.8502e-05 au
  Orbit Determination Parameters
   # obs. used (total)      146  
   data-arc span      119 days  
   first obs. used      2016-05-11  
   last obs. used      2016-09-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .49677  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:54  

Additional Information
 Earth MOID = .000914389 au 
 Jupiter MOID = 2.22984 au 
 T_jup = 3.703 
[ 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 24.7   n/a E2016R87  

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