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(2016 UC107)
Classification: Apollo [NEO]          SPK-ID: 3763100
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5901726978568332 0.00044135  
a 2.00876750918802 0.0019121 au
q .8232477689233751 0.00010296 au
i 2.02808391155966 0.0013997 deg
node 212.0360534756143 0.00052972 deg
peri 247.4638128951111 0.0016759 deg
M 77.36808855874474 0.62439 deg
tp 2458777.012979088243
(2019-Oct-20.51297909)
1.4845 TDB
period 1039.903260207128
2.85
1.4848
0.004065
d
yr
n .3461860480447914 0.00049429 deg/d
Q 3.194287249452664 0.0030406 au
  Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      4 days  
   first obs. used      2016-10-30  
   last obs. used      2016-11-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34526  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:22:34  

Additional Information
 Earth MOID = .00627993 au 
 Jupiter MOID = 2.01096 au 
 T_jup = 3.593 
[ 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 25.6   n/a MPO389558  

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