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14942 Stevebaker (1995 MA)
Classification: Main-belt Asteroid          SPK-ID: 2014942
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2457600.5 (2016-Jul-31.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0877817814508639 5.2295e-08  
a 3.186510733994621 2.7527e-08 au
q 2.906793145152273 1.6303e-07 au
i 15.78113233024328 6.5465e-06 deg
node 202.2368980785121 2.0967e-05 deg
peri 228.8967048500249 4.844e-05 deg
M 83.29913930899801 4.0347e-05 deg
tp 2457119.760819473038
(2015-Apr-07.26081947)
0.00023456 JED
period 2077.645776719469
5.69
2.6922e-05
7.371e-08
d
yr
n .1732730401081302 2.2453e-09 deg/d
Q 3.466228322836968 2.9943e-08 au
  Orbit Determination Parameters
   # obs. used (total)      936  
   data-arc span      8919 days (24.42 yr)  
   first obs. used      1991-10-10  
   last obs. used      2016-03-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-BIG16  
   condition code      0  
   fit RMS      .54838  
   data source      ORB  
   producer      Otto Matic  
   solution date      2016-Mar-24 16:21:49  

Additional Information
 Earth MOID = 1.94225 au 
 Jupiter MOID = 1.94757 au 
 T_jup = 3.133 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 13.4 mag n/a MPO365431  

14942 Stevebaker           Discovered 1995 June 21 by AMOS at Haleakala.
Steve Baker (b. 1967), a key member of the Air Force Maui Optical and Supercomputing (AMOS) team, provided support in computer security and has helped to make the annual AMOS Technical Conference a success.
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character)
Reference: 20050125/MPCPages.arcLast Updated: 2005-06-01

Alternate Designations
 1995 MA = 2000 GO59 
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Discovery Circumstances ]
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