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86578 (2000 EE48)
Classification: Main-belt Asteroid          SPK-ID: 2086578
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07745643047333643 3.5992e-08  
a 2.189449389705123 6.9058e-09 au
q 2.019862455276539 7.8222e-08 au
i 5.538791285210669 4.1493e-06 deg
node 5.71883693585927 3.7626e-05 deg
peri 185.8847427570666 4.5433e-05 deg
M 82.41927796014353 2.5982e-05 deg
tp 2458729.588714107476
(2019-Sep-03.08871411)
8.5238e-05 TDB
period 1183.316152908686
3.24
5.5985e-06
1.533e-08
d
yr
n .3042297691239076 1.4394e-09 deg/d
Q 2.359036324133707 7.4407e-09 au
  Orbit Determination Parameters
   # obs. used (total)      917  
   data-arc span      7495 days (20.52 yr)  
   first obs. used      2000-03-04  
   last obs. used      2020-09-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54187  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 20:56:50  

Additional Information
 Earth MOID = 1.01967 au 
 Jupiter MOID = 2.59803 au 
 T_jup = 3.664 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457426.5 (2016-Feb-08.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0777406198581168 3.6043e-08  
q 2.018932745762251 7.8437e-08 au
tp 2457545.795581077991
(2016-Jun-06.29558108)
8.4183e-05 TDB
node 5.752056084827342 3.7616e-05 deg
peri 185.5505941419065 4.5351e-05 deg
i 5.540220209882164 4.1498e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      917  
   data-arc span      7495 days (20.52 yr)  
   first obs. used      2000-03-04  
   last obs. used      2020-09-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54187  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 20:56:50  

Additional Information
 Jupiter MOID = 2.59803 au 
 T_jup = 3.664 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.299066512441458E-15 -2.817855581319715E-15 -1.604161884009165E-12 -3.54394362387421E-15 -4.85261747197519E-13 2.7198920146419E-16
q -2.817855581319715E-15 6.152410224802153E-15 3.551266469914798E-12 7.978344971531352E-15 1.07260168711136E-12 -5.440786754968774E-16
tp -1.604161884009165E-12 3.551266469914798E-12 7.086730141741651E-9 6.031268914837789E-12 2.145341661129432E-9 -8.525888580673144E-14
node -3.54394362387421E-15 7.978344971531352E-15 6.031268914837789E-12 1.414967444788176E-9 -1.406321513315002E-9 -7.917523213885516E-11
peri -4.85261747197519E-13 1.07260168711136E-12 2.145341661129432E-9 -1.406321513315002E-9 2.056708322824933E-9 7.880755722336477E-11
i 2.7198920146419E-16 -5.440786754968774E-16 -8.525888580673144E-14 -7.917523213885516E-11 7.880755722336477E-11 1.722053239249144E-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 16.1   n/a MPO426536  

86578 (2000 EE48)          Discovered 2000-Mar-09 by LINEAR at Socorro
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

[ 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
2066-Feb-07 07:47 00:02 Vesta 0.0435322305164992 0.0435258491407837 0.0435386127320097 3.50220682513169 3.50220604468737 2475688.824446736 2.00376233654017 436.985821019406 28.8616857706807 -43.6932246216938 155385.108800053 T 22 CATAB v2.0f-lin.ifort 2020-Nov-12 20:56:54 2020-Nov-12 20:56

Alternate Designations
 2000 EE48 = 2001 QP237 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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