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48326 (2002 NE47)
Classification: Main-belt Asteroid          SPK-ID: 2048326
[ 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 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0345674272000679 5.7582e-08  
a 2.550197114041005 1.3574e-08 au
q 2.46204336095557 1.5237e-07 au
i 13.66957949576653 4.2282e-06 deg
node 300.7892467732832 2.2301e-05 deg
peri 212.3839460457254 7.1073e-05 deg
M 288.3543348928872 6.6968e-05 deg
tp 2459296.537323948995
(2021-Mar-23.03732395)		 0.00027653 TDB
period 1487.507115221934
4.07		 1.1876e-05
3.251e-08		 d
yr
n .2420156490789548 1.9323e-09 deg/d
Q 2.638350867126441 1.4043e-08 au
   Orbit Determination Parameters
   # obs. used (total)      1171  
   data-arc span      8143 days (22.29 yr)  
   first obs. used      1998-08-01  
   last obs. used      2020-11-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49497  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-17 21:26:10  

Additional Information
 Earth MOID = 1.4826 au 
 Jupiter MOID = 2.42699 au 
 T_jup = 3.400 
[ 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 14.3   n/a MPO452829  
diameter diameter 4.695 km 0.097 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.184   0.024 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

48326 (2002 NE47)          Discovered 2002-Jul-13 by NEAT at Haleakala
Reference: 20020921/Numbers.arcLast Updated: 2004-04-19

[ 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
1919-Jan-14 22:29 00:03 Vesta 0.0282178169926864 0.0282139547596351 0.0282216974183244 6.8360232885465 6.83602267171341 2421973.436814772 3.12519537400193 1166.32132431153 37.5773103287773 80.6649580426322 110684.888447903 T 26 CATAB v2.0f-lin.ifort 2020-Dec-17 21:26:13 2020-Dec-17 21:26
2085-Dec-18 16:52 00:03 Vesta 0.0484827685557635 0.0484737675165287 0.0484917757705925 6.81113222462197 6.81113186430237 2482943.202698306 2.90869858230898 973.984698317613 37.7037626286719 -62.675790603322 170682.576553862 T 26 CATAB v2.0f-lin.ifort 2020-Dec-17 21:26:13 2020-Dec-17 21:26
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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