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(2017 YP6)
Classification: Apollo [NEO]          SPK-ID: 3795108
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 2458116.5 (2017-Dec-29.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3528387830669935 0.0012454  
a 1.520825265305562 0.0030232 au
q .9842191294376101 6.5198e-05 au
i 27.1448531695614 0.048829 deg
node 96.09547596698015 6.0166e-05 deg
peri 30.64033841544379 0.036137 deg
M 346.4982096103441 0.061575 deg
tp 2458142.192494116755
(2018-Jan-23.69249412)
0.040856 TDB
period 685.042325136223
1.88
2.0427
0.005593
d
yr
n .5255149744629469 0.001567 deg/d
Q 2.057431401173514 0.0040899 au
  Orbit Determination Parameters
   # obs. used (total)      28  
   data-arc span      1 day  
   first obs. used      2017-12-28  
   last obs. used      2017-12-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .50909  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Dec-29 14:12:05  

Additional Information
 Earth MOID = .0364278 au 
 Jupiter MOID = 3.12814 au 
 T_jup = 4.322 
[ 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 25.1   n/a MPO431432  

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