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129063 Joshwood (2004 VF26)
Classification: Main-belt Asteroid          SPK-ID: 2129063
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 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05740598103228495 4.8126e-08  
a 3.115162610894024 3.9758e-08 au
q 2.936333645140559 1.4541e-07 au
i 8.22290451003672 5.2161e-06 deg
node 248.5445983296261 3.8875e-05 deg
peri 178.7425150862725 6.4683e-05 deg
M 282.4598031451001 5.0505e-05 deg
tp 2459433.057561071752
(2021-Aug-06.55756107)
0.00028239 TDB
period 2008.258017157592
5.50
3.8446e-05
1.053e-07
d
yr
n .1792598346050821 3.4318e-09 deg/d
Q 3.29399157664749 4.204e-08 au
  Orbit Determination Parameters
   # obs. used (total)      626  
   data-arc span      7175 days (19.64 yr)  
   first obs. used      1998-09-25  
   last obs. used      2018-05-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55427  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-May-31 16:09:53  

Additional Information
 Earth MOID = 1.95021 au 
 Jupiter MOID = 1.96311 au 
 T_jup = 3.199 
[ 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 14.5   n/a MPO401138  

129063 Joshwood           Discovered 2004 Nov. 4 by the Catalina Sky Survey.
Josh Wood (b. 1977) is the flight system System Design Lead and CPE at Lockheed Martin for the OSIRIS-REx Asteroid Sample Return Mission. He was also Systems/Electrical/Payload Accommodations Engineer for the GRAIL program, and the STL lead for the Phoenix Mars Lander.
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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