Skip Page Navigation
NASA JPL Caltech
NASA Logo - Jet Propulsion Laboratory + View the NASA Portal
+ Center for Near-Earth Object Studies
JPL Home Earth Solar System Stars & Galaxies Technology
JPL Solar System Dynamics
BODIES ORBITS EPHEMERIDES TOOLS PHYSICAL DATA DISCOVERY FAQ SITE MAP
JPL Small-Body Database Browser
Search: [ help ]  
469462 (2002 QF106)
Classification: Main-belt Asteroid          SPK-ID: 2469462
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1829362070077137 1.2853e-07  
a 2.286551232510027 1.6405e-08 au
q 1.86825822290583 2.8927e-07 au
i 5.473655963403637 8.0543e-06 deg
node 73.42984731077158 0.00011236 deg
peri 279.2845287218843 0.0001147 deg
M 37.2098449424336 2.1584e-05 deg
tp 2458869.965535663940
(2020-Jan-21.46553566)
7.5211e-05 TDB
period 1262.902525761192
3.46
1.3591e-05
3.721e-08
d
yr
n .2850576292758749 3.0678e-09 deg/d
Q 2.704844242114224 1.9406e-08 au
  Orbit Determination Parameters
   # obs. used (total)      77  
   data-arc span      5640 days (15.44 yr)  
   first obs. used      2002-08-12  
   last obs. used      2018-01-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .61289  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Feb-06 09:56:56  

Additional Information
 Earth MOID = .872632 au 
 Jupiter MOID = 2.74097 au 
 T_jup = 3.573 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457036.5 (2015-Jan-14.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1838266084804186 1.2849e-07  
q 1.866005539506849 2.8927e-07 au
tp 2457607.633614960753
(2016-Aug-07.13361496)
7.1025e-05 TDB
node 73.4435845814555 0.00011238 deg
peri 279.4427788570872 0.0001147 deg
i 5.473956817323496 8.059e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      77  
   data-arc span      5640 days (15.44 yr)  
   first obs. used      2002-08-12  
   last obs. used      2018-01-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .61289  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Feb-06 09:56:56  

Additional Information
 Jupiter MOID = 2.74097 au 
 T_jup = 3.573 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.651001460900747E-14 -3.713394697162213E-14 2.864461408012791E-12 -2.196901395047758E-13 3.996645097508467E-13 -7.277106094911165E-14
q -3.713394697162213E-14 8.367725344109185E-14 -6.395894551209097E-12 4.931611500315533E-13 -9.098468316991863E-13 1.636831368519877E-13
tp 2.864461408012791E-12 -6.395894551209097E-12 5.044481174581924E-9 -8.786827456448061E-11 1.715161659672117E-9 -1.878491291027181E-11
node -2.196901395047758E-13 4.931611500315533E-13 -8.786827456448061E-11 1.263016148443411E-8 -1.259357101933653E-8 -4.702719240977629E-10
peri 3.996645097508467E-13 -9.098468316991863E-13 1.715161659672117E-9 -1.259357101933653E-8 1.315604986294754E-8 4.655328152848072E-10
i -7.277106094911165E-14 1.636831368519877E-13 -1.878491291027181E-11 -4.702719240977629E-10 4.655328152848072E-10 6.494749260076995E-11

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 17.8   n/a MPO434687  

469462 (2002 QF106)          Discovered 2002-Aug-19 by NEAT at Palomar
Reference: Last Updated: 2016-08-22
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Jul-06 16:36 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin