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JPL Small-Body Database Browser
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32966 (1996 PE5)
Classification: Main-belt Asteroid          SPK-ID: 2032966
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1583734175277057 3.6664e-08  
a 2.452404200414758 1.3301e-08 au
q 2.064008566035772 8.812e-08 au
i 6.634686213958863 6.29e-06 deg
node 331.3820023438331 3.2363e-05 deg
peri 262.3722614835938 3.8875e-05 deg
M 52.79765124252868 2.2276e-05 deg
tp 2458394.769535809386
(2018-Oct-03.26953581)
8.643e-05 TDB
period 1402.770111276526
3.84
1.1412e-05
3.124e-08
d
yr
n .2566350659356427 2.0878e-09 deg/d
Q 2.840799834793744 1.5407e-08 au
  Orbit Determination Parameters
   # obs. used (total)      726  
   data-arc span      8449 days (23.13 yr)  
   first obs. used      1996-08-15  
   last obs. used      2019-10-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56011  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 05:28:30  

Additional Information
 Earth MOID = 1.06591 au 
 Jupiter MOID = 2.20679 au 
 T_jup = 3.468 
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Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.4   n/a MPO351058  

32966 (1996 PE5)          Discovered 1996-Aug-15 by Viscome, G. R. at Rand
Reference: 20020128/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1996 PE5 = 1999 FB34 = 1999 GE52 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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