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(2003 FY6)
Classification: Aten [NEO]          SPK-ID: 3151655
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2456876.5 (2014-Aug-07.0) TDB
Reference: JPL 35 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .581973191827923 8.4972e-07  
a .7300146112084784 3.3383e-09 au
q .30516567784246 6.2154e-07 au
i 6.606160166273198 3.6489e-05 deg
node 359.3058651656581 4.9243e-05 deg
peri 29.54119134882719 3.7164e-05 deg
M 184.4919750728291 0.00016543 deg
tp 2456987.568327945237
(2014-Nov-26.06832795)
0.00010406 TDB
period 227.8220501705116
0.62
1.5627e-06
4.278e-09
d
yr
n 1.580180670530183 1.0839e-08 deg/d
Q 1.154863544574497 5.2811e-09 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] -6.346293837877295E-14 1.336E-14
ALN [SET] 1. n/a
NK [SET] 0. n/a
NM [SET] 2. n/a
R0 [SET] 1. n/a
  Orbit Determination Parameters
   # obs. used (total)      182  
   data-arc span      5497 days (15.05 yr)  
   first obs. used      2003-03-29  
   last obs. used      2018-04-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .36618  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jan-14 15:32:06  

Additional Information
 Earth MOID = .00352385 au 
 Jupiter MOID = 4.29918 au 
 T_jup = 7.733 
 Nongravitational accels. using nonstandard g(r) = (1 au/ r)^2 
[ 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 22.4   n/a MPO266873  

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