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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 ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .158373417943343 3.6579e-08  
a 2.45240420019281 1.3226e-08 au
q 2.064008564829664 8.7818e-08 au
i 6.63468687187169 6.2438e-06 deg
node 331.3819980371904 3.1977e-05 deg
peri 262.3722661286275 3.8505e-05 deg
M 52.79765097066048 2.2256e-05 deg
tp 2458394.769536896671
(2018-Oct-03.26953690)
8.6345e-05 TDB
period 1402.770111086095
3.84
1.1348e-05
3.107e-08
d
yr
n .2566350659704818 2.0761e-09 deg/d
Q 2.840799835555956 1.5321e-08 au
  Orbit Determination Parameters
   # obs. used (total)      730  
   data-arc span      8492 days (23.25 yr)  
   first obs. used      1996-08-15  
   last obs. used      2019-11-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55942  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 02:29:49  

Additional Information
 Earth MOID = 1.06591 au 
 Jupiter MOID = 2.20679 au 
 T_jup = 3.468 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457050.5 (2015-Jan-28.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .15761432434322 3.6577e-08  
q 2.066016259308693 8.7773e-08 au
tp 2456992.033636823283
(2014-Nov-30.53363682)
8.511e-05 TDB
node 331.4339569095263 3.197e-05 deg
peri 262.4337047063777 3.8549e-05 deg
i 6.635081840497113 6.2436e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      730  
   data-arc span      8492 days (23.25 yr)  
   first obs. used      1996-08-15  
   last obs. used      2019-11-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55942  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 02:29:49  

Additional Information
 Jupiter MOID = 2.20679 au 
 T_jup = 3.468 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.337888019739029E-15 -3.186126469596757E-15 4.658351555201752E-13 -6.038700730522434E-15 6.390844644202535E-14 1.932845020345228E-15
q -3.186126469596757E-15 7.70402395773908E-15 -1.07051221781828E-12 1.40192831038726E-14 -1.414649405997344E-13 -4.593440681684249E-15
tp 4.658351555201752E-13 -1.07051221781828E-12 7.243653534698814E-9 -1.690576732502269E-11 1.83792539250831E-9 -3.187446615564439E-12
node -6.038700730522434E-15 1.40192831038726E-14 -1.690576732502269E-11 1.022099688633589E-9 -1.018619195053402E-9 -2.148372753935964E-11
peri 6.390844644202535E-14 -1.414649405997344E-13 1.83792539250831E-9 -1.018619195053402E-9 1.486050943705016E-9 2.04271275177859E-11
i 1.932845020345228E-15 -4.593440681684249E-15 -3.187446615564439E-12 -2.148372753935964E-11 2.04271275177859E-11 3.898272958923836E-11

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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