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(2017 UU2)
Classification: Apollo [NEO]          SPK-ID: 3787627
[ 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 2458048.5 (2017-Oct-22.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5263625253448203 0.00086614  
a 1.819500155720445 0.0030136 au
q .8617834588901376 0.00014858 au
i 1.685798761567542 0.0021651 deg
node 221.5927729746811 0.0028228 deg
peri 222.030755969554 0.001801 deg
M 343.6611211492022 0.046668 deg
tp 2458089.186124557844
(2017-Dec-01.68612456)		 0.015127 TDB
period 896.451034038276
2.45		 2.2272
0.006098		 d
yr
n .4015835626607454 0.00099771 deg/d
Q 2.777216852550752 0.0045999 au
   Orbit Determination Parameters
   # obs. used (total)      28  
   data-arc span      3 days  
   first obs. used      2017-10-21  
   last obs. used      2017-10-24  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .2945  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Oct-24 06:21:51  

Additional Information
 Earth MOID = .00516055 au 
 Jupiter MOID = 2.49133 au 
 T_jup = 3.865 
[ 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 26.4   n/a MPO421535  

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