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(2004 FU162)
Classification: Aten [NEO]          SPK-ID: 3249978
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2453100.5 (2004-Apr-05.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3921712395216529 0.039142  
a .8268612736523362 0.11089 au
q .5025900630516469 0.041873 au
i 4.164680034919877 2.9908 deg
node 191.2486004165659 0.091892 deg
peri 139.7843002537736 22.242 deg
M 262.6667234495233 38.186 deg
tp 2453174.751673713520
(2004-Jun-18.25167371)
14.287 TDB
period 274.6296383334512
0.75
55.246
0.1513
d
yr
n 1.310856330673579 0.2637 deg/d
Q 1.151132484253026 0.15438 au
  Orbit Determination Parameters
   # obs. used (total)      4  
   first obs. used      2004-03-31  
   last obs. used      2004-03-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .14946  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:12:58  

Additional Information
 Earth MOID = 7.22621E-5 au 
 Jupiter MOID = 4.17971 au 
 T_jup = 7.024 
[ 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 28.7   n/a MPO66355  

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2004-Mar-31 12:42 02:31 Moon 0.00256565286087296 0.00253787872242191 0.00259623166238724 12.0702121075063 12.0691537679837 2453096.028993781 150.620772407252 4475.48934941843 44.6773163185651 -71.2389436451706 360.028065883235 T 10 CATAB v2.0e-lin.ifort 2017-Nov-27 22:32:42 2018-Dec-11 14:43
2004-Mar-31 15:35 01:32 Earth 8.63186539409982e-05 2.31892328201605e-05 0.000196405434560326 13.3906295084675 10.8431117084454 2453096.149229127 91.6479703439146 5301.66784475839 688.556649908627 -35.9194481978357 1.14907545728789 T 10 CATAB v2.0e-lin.ifort 2017-Nov-27 22:32:42 2018-Dec-11 14:43
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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