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JPL Small-Body Database Browser
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136582 (1992 BA)
Classification: Amor [NEO]          SPK-ID: 2136582
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 102 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06782803206613811 3.2589e-08  
a 1.341778964979367 7.1934e-09 au
q 1.250768738317077 4.9157e-08 au
i 10.49794588371675 4.2723e-06 deg
node 140.188735205801 1.1101e-05 deg
peri 107.4445708709888 3.5658e-05 deg
M 328.8326812176973 3.6144e-05 deg
tp 2459049.649243531264
(2020-Jul-19.14924353)
5.7229e-05 TDB
period 567.7013090167326
1.55
4.5652e-06
1.25e-08
d
yr
n .6341362866038227 5.0995e-09 deg/d
Q 1.432789191641657 7.6813e-09 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] -5.356922915204884E-14 1.667E-14
ALN [SET] 1. n/a
NK [SET] 0. n/a
NM [SET] 2. n/a
R0 [SET] 1. n/a
  Orbit Determination Parameters
   # obs. used (total)      408  
   data-arc span      10320 days (28.25 yr)  
   first obs. used      1992-01-27  
   last obs. used      2020-04-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50217  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 22:39:43  

Additional Information
 Earth MOID = .275516 au 
 Jupiter MOID = 3.57343 au 
 T_jup = 4.874 
 Nongravitational accels. using nonstandard g(r) = (1 au/ r)^2 
[ 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 19.9   n/a MPO417722  

136582 (1992 BA)          Discovered 1992-Jan-27 by Spacewatch at Kitt Peak
Reference: 20061205/Numbers.arcLast Updated: 2006-12-13

[ show close-approach data ]
Alternate Designations
 1992 BA = 2000 PN3 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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