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67085 Oppenheimer (2000 AG42)
Classification: Main-belt Asteroid          SPK-ID: 2067085
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1703813616160903 3.6415e-08  
a 2.359410660731108 1.0794e-08 au
q 1.957411059744223 9.0398e-08 au
i .693587341054251 4.063e-06 deg
node 232.5304962147129 0.00033884 deg
peri 210.5652661603893 0.00033942 deg
M 353.4897238034349 2.4371e-05 deg
tp 2459420.438704618270
(2021-Jul-24.93870462)
8.9747e-05 TDB
period 1323.743171929314
3.62
9.0843e-06
2.487e-08
d
yr
n .2719560770049611 1.8663e-09 deg/d
Q 2.761410261717994 1.2634e-08 au
  Orbit Determination Parameters
   # obs. used (total)      503  
   data-arc span      9170 days (25.11 yr)  
   first obs. used      1995-10-03  
   last obs. used      2020-11-10  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .56656  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 12:27:13  

Additional Information
 Earth MOID = .973404 au 
 Jupiter MOID = 2.45923 au 
 T_jup = 3.532 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457598.5 (2016-Jul-29.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1710305983884858 3.6819e-08  
q 1.955931930295855 9.1686e-08 au
tp 2458093.229776110223
(2017-Dec-05.72977611)
8.1629e-05 TDB
node 232.6405392969533 0.0003385 deg
peri 209.7901394029185 0.00033908 deg
i .6935009217120556 4.0685e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      503  
   data-arc span      9170 days (25.11 yr)  
   first obs. used      1995-10-03  
   last obs. used      2020-11-10  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .56656  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 12:27:13  

Additional Information
 Jupiter MOID = 2.45923 au 
 T_jup = 3.532 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.355610646927753E-15 -3.362430710978142E-15 -1.38815404534953E-12 -9.00046927799826E-16 -3.107618914058436E-13 -2.911572472660095E-16
q -3.362430710978142E-15 8.406355087338586E-15 3.879061770250955E-12 4.423667193398503E-15 8.723982023326206E-13 8.341867660245591E-16
tp -1.38815404534953E-12 3.879061770250955E-12 6.663353798422549E-9 1.732040899297565E-11 1.627665690572596E-9 1.253920973809328E-12
node -9.00046927799826E-16 4.423667193398503E-15 1.732040899297565E-11 1.145823233822217E-7 -1.145694482825864E-7 -3.240908607976908E-10
peri -3.107618914058436E-13 8.723982023326206E-13 1.627665690572596E-9 -1.145694482825864E-7 1.149731615230502E-7 3.243720042651969E-10
i -2.911572472660095E-16 8.341867660245591E-16 1.253920973809328E-12 -3.240908607976908E-10 3.243720042651969E-10 1.65529266990683E-11

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.89   n/a MPCxxxxx  

67085 Oppenheimer           Discovered 2000 Jan. 4 by S. Sposetti at Gnosca.
J. Robert Oppenheimer (1904-1967) was a theoretical physicist and the scientific director of the Manhattan Project. From 1947 to 1966 he directed the Institute of Advanced Study at Princeton.
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character)
Reference: 20061109/MPCPages.arcLast Updated: 2006-11-13

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Alternate Designations
 2000 AG42 = 2002 RY162 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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