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347546 (2000 EE132)
Classification: Main-belt Asteroid          SPK-ID: 2347546
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09588794734726477 6.5191e-08  
a 2.736387424596407 2.7158e-08 au
q 2.474000851304989 1.808e-07 au
i 5.06958420031806 7.1334e-06 deg
node 13.94599093887965 7.0645e-05 deg
peri 155.2638848531824 8.1229e-05 deg
M 177.9758655170301 3.618e-05 deg
tp 2458183.121107434741
(2018-Mar-05.62110743)
0.00016666 TDB
period 1653.350022873392
4.53
2.4614e-05
6.739e-08
d
yr
n .2177397375144729 3.2415e-09 deg/d
Q 2.998773997887824 2.9762e-08 au
  Orbit Determination Parameters
   # obs. used (total)      160  
   data-arc span      7066 days (19.35 yr)  
   first obs. used      2000-02-27  
   last obs. used      2019-07-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58559  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-24 06:33:41  

Additional Information
 Earth MOID = 1.48087 au 
 Jupiter MOID = 1.96698 au 
 T_jup = 3.340 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457262.5 (2015-Aug-28.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09386536258836847 6.5453e-08  
q 2.481497170114999 1.8133e-07 au
tp 2456527.334801128037
(2013-Aug-22.83480113)
0.00017456 TDB
node 14.06911829609255 7.0526e-05 deg
peri 155.2308878544887 8.1526e-05 deg
i 5.073219093078126 7.1356e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      160  
   data-arc span      7066 days (19.35 yr)  
   first obs. used      2000-02-27  
   last obs. used      2019-07-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58559  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-24 06:33:41  

Additional Information
 Jupiter MOID = 1.96698 au 
 T_jup = 3.340 
Orbit Covariance (6×6)
  e q tp node peri i
e 4.284099953531459E-15 -1.175861734346391E-14 4.829772625069683E-13 -2.651607058390647E-14 1.337831841180262E-13 -4.156999521884052E-15
q -1.175861734346391E-14 3.288126104888872E-14 -2.276888622655581E-12 6.774963441636362E-14 -5.276220914686032E-13 1.233793322948983E-14
tp 4.829772625069683E-13 -2.276888622655581E-12 3.047048243367469E-8 9.477060434290044E-12 7.163946311433927E-9 -3.266885226117396E-12
node -2.651607058390647E-14 6.774963441636362E-14 9.477060434290044E-12 4.973926121636072E-9 -4.951628195692476E-9 -6.714101235682625E-11
peri 1.337831841180262E-13 -5.276220914686032E-13 7.163946311433927E-9 -4.951628195692476E-9 6.646520689567934E-9 6.627842672273959E-11
i -4.156999521884052E-15 1.233793322948983E-14 -3.266885226117396E-12 -6.714101235682625E-11 6.627842672273959E-11 5.091646199516678E-11

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 16.5   n/a MPO437471  

347546 (2000 EE132)          Discovered 2000-Mar-11 by LINEAR at Socorro
Reference: 20121228/Numbers.arcLast Updated: 2013-01-02

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
1975-May-24 01:57 00:02 Jupiter 1.97039350006076 1.97039291162109 1.97039408850031 3.05602314347775 2.91196288598629 2442556.581014475 1.67582610566875 125.317771777315 20.4819125171098 89.3972281841852 1936690.01881421 T 9 CATAB v2.0f-lin.ifort 2019-Sep-24 06:33:42 2019-Sep-24 06:33
2033-Dec-06 07:23 < 00:01 Jupiter 1.99748528531785 1.99748467153516 1.99748589910054 3.05265849918748 2.91043554233558 2463937.807846346 0.885646059279376 91.8929986571441 22.0343476424658 -87.3157225808534 2108952.11997224 T 9 CATAB v2.0f-lin.ifort 2019-Sep-24 06:33:42 2019-Sep-24 06:33
2070-Sep-04 02:18 00:02 Jupiter 1.99385965419446 1.99385888094262 1.99386042744653 3.12738740400168 2.98846464672642 2477358.595513504 2.38529186201064 124.140843441712 26.5963672643794 85.4522706659402 1898884.85119314 T 9 CATAB v2.0f-lin.ifort 2019-Sep-24 06:33:42 2019-Sep-24 06:33
2129-Mar-21 00:08 00:05 Jupiter 1.96460952411519 1.96460878950189 1.96461025873821 3.0116088779908 2.86487473628773 2498740.505472461 4.84369957931307 331.263062352421 19.1195068387199 -86.1453122614756 1980874.33208848 T 9 CATAB v2.0f-lin.ifort 2019-Sep-24 06:33:42 2019-Sep-24 06:33
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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