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 ]  
86516 (2000 DT67)
Classification: Main-belt Asteroid          SPK-ID: 2086516
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 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1353473345482503 3.7855e-08  
a 2.33553258453968 9.457e-09 au
q 2.019424474471649 9.0593e-08 au
i 6.165378794528056 4.2104e-06 deg
node 187.7625270298229 3.2333e-05 deg
peri 143.2889769388394 3.7047e-05 deg
M 79.59267358654067 1.5168e-05 deg
tp 2458712.264203528889
(2019-Aug-16.76420353)
5.527e-05 TDB
period 1303.698971950943
3.57
7.9184e-06
2.168e-08
d
yr
n .2761373658684962 1.6772e-09 deg/d
Q 2.651640694607712 1.0737e-08 au
  Orbit Determination Parameters
   # obs. used (total)      738  
   data-arc span      7726 days (21.15 yr)  
   first obs. used      1998-11-11  
   last obs. used      2020-01-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50669  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-29 13:27:41  

Additional Information
 Earth MOID = 1.01314 au 
 Jupiter MOID = 2.69745 au 
 T_jup = 3.548 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457255.5 (2015-Aug-21.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1362201301765352 3.7967e-08  
q 2.017170294438267 9.1001e-08 au
tp 2457409.358348320812
(2016-Jan-21.85834832)
5.6978e-05 TDB
node 187.7989554426139 3.2306e-05 deg
peri 143.4621082974947 3.6956e-05 deg
i 6.168014509490053 4.2128e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      738  
   data-arc span      7726 days (21.15 yr)  
   first obs. used      1998-11-11  
   last obs. used      2020-01-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50669  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-29 13:27:41  

Additional Information
 Jupiter MOID = 2.69745 au 
 T_jup = 3.548 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.44147691423507E-15 -3.441665533227428E-15 7.996515328385095E-13 -1.386707155736046E-15 2.769112350202393E-13 -2.62566851429722E-16
q -3.441665533227428E-15 8.281235971522153E-15 -2.031766610922506E-12 3.144312711110124E-15 -7.014369592751173E-13 5.454775328392209E-16
tp 7.996515328385095E-13 -2.031766610922506E-12 3.246510827774651E-9 -1.0609663551181E-11 1.030854076227295E-9 3.622346677096313E-12
node -1.386707155736046E-15 3.144312711110124E-15 -1.0609663551181E-11 1.043677473040765E-9 -1.040292744812467E-9 -9.494293256483173E-13
peri 2.769112350202393E-13 -7.014369592751173E-13 1.030854076227295E-9 -1.040292744812467E-9 1.365770341095163E-9 2.041544821438875E-12
i -2.62566851429722E-16 5.454775328392209E-16 3.622346677096313E-12 -9.494293256483173E-13 2.041544821438875E-12 1.77480007701473E-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 15.8   n/a MPO439621  

86516 (2000 DT67)          Discovered 2000-Feb-29 by LINEAR at Socorro
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

Alternate Designations
 2000 DT67 = 2004 FY64 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Oct-27 02:27 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin