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129051 Chrismay (2004 VO10)
Classification: Main-belt Asteroid          SPK-ID: 2129051
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 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06617860052794167 9.887e-08  
a 3.001163462822638 3.1835e-08 au
q 2.802550664897444 3.0589e-07 au
i 9.842525902959107 1.0088e-05 deg
node 342.3300873237729 2.6305e-05 deg
peri 348.8607681397471 5.5006e-05 deg
M 64.53191718246273 4.6011e-05 deg
tp 2458660.087914912497
(2019-Jun-25.58791491)
0.00024489 TDB
period 1899.034709986966
5.20
3.0216e-05
8.273e-08
d
yr
n .1895699947487905 3.0163e-09 deg/d
Q 3.199776260747831 3.3942e-08 au
  Orbit Determination Parameters
   # obs. used (total)      376  
   data-arc span      8674 days (23.75 yr)  
   first obs. used      1996-02-15  
   last obs. used      2019-11-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57642  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 10:34:15  

Additional Information
 Earth MOID = 1.79296 au 
 Jupiter MOID = 2.14691 au 
 T_jup = 3.227 
[ 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 15.1   n/a MPO493738  

129051 Chrismay           Discovered 2004 Nov. 3 by the Catalina Sky Survey.
Chris May (b. 1972) is the Thermal Lead for the OSIRIS-REx spacecraft. He was the Thermal Lead for the GRAIL lunar mission and thermal engineer on the Mars Phoenix lander, Mars Reconnaissance Orbiter and Mars Odyssey missions.
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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