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129050 Lowellcogburn (2004 VW9)
Classification: Main-belt Asteroid          SPK-ID: 2129050
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1313593225409913 4.7768e-08  
a 2.782402352642749 1.885e-08 au
q 2.416907864563137 1.3249e-07 au
i 14.79338711512164 5.9755e-06 deg
node 342.5044059508278 1.7985e-05 deg
peri 91.86591608067087 3.3903e-05 deg
M 96.60233605046008 2.5678e-05 deg
tp 2458545.602602065840
(2019-Mar-03.10260207)
0.00012058 TDB
period 1695.228810727271
4.64
1.7227e-05
4.716e-08
d
yr
n .2123607136228154 2.1581e-09 deg/d
Q 3.14789684072236 2.1326e-08 au
  Orbit Determination Parameters
   # obs. used (total)      428  
   data-arc span      7494 days (20.52 yr)  
   first obs. used      1999-10-13  
   last obs. used      2020-04-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55892  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 21:41:36  

Additional Information
 Earth MOID = 1.48602 au 
 Jupiter MOID = 2.17353 au 
 T_jup = 3.272 
[ show covariance matrix ]

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 15.7   n/a MPO469346  
diameter diameter 2.146 km 0.855 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.167   0.123 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

129050 Lowellcogburn           Discovered 2004 Nov. 3 by the Catalina Sky Survey.
Lowell Cogburn (b. 1955) is the OSIRIS REx spacecraft lead dynamics analyst responsible for Touch and Go dynamic analysis and Sample Return Capsule release dynamic analysis. He was the Dynamics lead on the GRAIL lunar mission.
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character)
Reference: MPC batch dated 2016-08-18Last Updated: 2016-08-22

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