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(2016 EB1)
Classification: Apollo [NEO]          SPK-ID: 3745026
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 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4460998953060875 0.00034  
a 1.34486860155887 0.0006129 au
q .7449228592030136 0.00011777 au
i 11.10720432500104 0.007791 deg
node 346.4893910099015 5.8055e-05 deg
peri 263.5122987312968 0.0032172 deg
M 220.9491308912556 0.64081 deg
tp 2459220.533808158431
(2021-Jan-06.03380816)
1.1644 TDB
period 569.6632566538473
1.56
0.38942
0.001066
d
yr
n .6319522907526262 0.000432 deg/d
Q 1.944814343914726 0.00088632 au
  Orbit Determination Parameters
   # obs. used (total)      69  
   data-arc span      10 days  
   first obs. used      2016-03-01  
   last obs. used      2016-03-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .38414  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Feb-10 07:07:38  

Additional Information
 Earth MOID = .0133271 au 
 Jupiter MOID = 3.16383 au 
 T_jup = 4.762 
[ 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 MPO438023  

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