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(2016 JB29)
Classification: Apollo [NEO]          SPK-ID: 3753295
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 43 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4948826880111596 6.6969e-06  
a 1.971461524466799 2.572e-05 au
q .9958193459280912 2.126e-07 au
i 6.277610173118068 5.792e-05 deg
node 82.19584073923107 2.6117e-05 deg
peri 199.1214347747933 1.0944e-05 deg
M 222.101822187373 0.011309 deg
tp 2459587.790560593977
(2022-Jan-08.29056059)
0.039341 TDB
period 1011.069210814944
2.77
0.019785
5.417e-05
d
yr
n .3560587110647272 6.9677e-06 deg/d
Q 2.947103703005508 3.8448e-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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      4  
   norm. resid. RMS      .49399  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 17:06:44  

Additional Information
 Earth MOID = .00190447 au 
 Jupiter MOID = 2.22923 au 
 T_jup = 3.703 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457548.5 (2016-Jun-09.0) TDB
Reference: JPL 43 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4952851355145577 6.6168e-06  
q .9962982398736278 1.8465e-07 au
tp 2457565.932371349506
(2016-Jun-26.43237135)
3.3567e-05 TDB
node 82.20912971642824 2.4742e-05 deg
peri 199.0800016866917 1.3511e-05 deg
i 6.278122825367219 5.7799e-05 deg
  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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      4  
   norm. resid. RMS      .49399  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 17:06:44  

Additional Information
 Jupiter MOID = 2.22923 au 
 T_jup = 3.703 
Orbit Covariance (6×6)
  e q tp node peri i
e 4.378143638142165E-11 -1.212157542152772E-12 -2.176906929803404E-10 1.587456596041549E-10 5.449233146489546E-11 3.819556044638024E-10
q -1.212157542152772E-12 3.409478270423437E-14 5.897053140873243E-12 -4.334750482575441E-12 -1.729773480694437E-12 -1.05942071439601E-11
tp -2.176906929803404E-10 5.897053140873243E-12 1.126749680145844E-9 -7.946381643123305E-10 -2.121129397117873E-10 -1.892583353606978E-9
node 1.587456596041549E-10 -4.334750482575441E-12 -7.946381643123305E-10 6.121596835546255E-10 1.545077600468421E-10 1.375417207731234E-9
peri 5.449233146489546E-11 -1.729773480694437E-12 -2.121129397117873E-10 1.545077600468421E-10 1.825454304950607E-10 4.927357383308424E-10
i 3.819556044638024E-10 -1.05942071439601E-11 -1.892583353606978E-9 1.375417207731234E-9 4.927357383308424E-10 3.34072690903221E-9

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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