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JPL Small-Body Database Browser
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351917 (2006 SL382)
Classification: Main-belt Asteroid          SPK-ID: 2351917
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1881165105868635 5.4208e-08  
a 3.014608701306199 4.2963e-08 au
q 2.447511031631681 1.6993e-07 au
i 11.03908335113529 1.1076e-05 deg
node 123.6773490085098 3.7008e-05 deg
peri 304.2311951372479 5.6811e-05 deg
M 120.7277587619882 3.5887e-05 deg
tp 2457959.364998584486
(2017-Jul-24.86499858)
0.00019079 TDB
period 1911.810530373704
5.23
4.087e-05
1.119e-07
d
yr
n .1883031787305985 4.0255e-09 deg/d
Q 3.581706370980717 5.1045e-08 au
  Orbit Determination Parameters
   # obs. used (total)      128  
   data-arc span      6357 days (17.40 yr)  
   first obs. used      2001-12-11  
   last obs. used      2019-05-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48667  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 09:27:11  

Additional Information
 Earth MOID = 1.48169 au 
 Jupiter MOID = 1.77512 au 
 T_jup = 3.194 
[ 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 16.5   n/a MPO437488  

351917 (2006 SL382)          Discovered 2006-Sep-28 by Becker, A. C. at Apache Point
Reference: 20130127/Numbers.arcLast Updated: 2013-01-31

[ 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
1936-Oct-16 21:09 00:05 Jupiter 1.79588157794502 1.79588042877615 1.79588272711797 2.56059463964987 2.36925104427258 2428458.381382593 5.37439340301596 387.075123876356 69.5667632393286 -82.151126317666 795089.102886725 T 6 CATAB v2.0e-lin.ifort 2019-May-30 09:27:12 2019-May-30 09:27
1983-Sep-10 09:23 00:02 Jupiter 1.85329319952483 1.85329210243211 1.85329429661861 2.15694292910947 1.93347612621278 2445587.890888836 2.30058580551232 262.979131402251 76.3780083987639 85.9462030173244 1250935.94998064 T 6 CATAB v2.0e-lin.ifort 2019-May-30 09:27:12 2019-May-30 09:27
2021-Jun-07 08:13 < 00:01 Jupiter 1.9510599594788 1.9510584674863 1.95106145147141 3.80528996400427 3.68943933849287 2459372.842048458 0.62678400869938 99.4276218964311 42.8150769442938 57.6957512394843 1051076.63426629 T 6 CATAB v2.0e-lin.ifort 2019-May-30 09:27:12 2019-May-30 09:27
2030-Jul-24 21:09 00:01 Jupiter 1.95887243324893 1.95887110953891 1.95887375695885 1.90222739103068 1.65941641668183 2462707.381210922 1.3990251743362 307.729970413959 69.2690798564024 85.0345275752317 1635390.98019887 T 6 CATAB v2.0e-lin.ifort 2019-May-30 09:27:12 2019-May-30 09:27
2068-May-07 02:49 00:04 Jupiter 1.82987210409439 1.82987025470329 1.82987395350172 3.35700425342139 3.21616311606255 2476508.617084186 3.55074203166061 369.732920670085 43.5467635321358 80.5022476515563 955393.424562917 T 6 CATAB v2.0e-lin.ifort 2019-May-30 09:27:12 2019-May-30 09:27
2115-Apr-11 21:49 00:07 Jupiter 1.77123208745162 1.77123075641071 1.77123341852394 2.99454346470576 2.83034781141866 2493648.408691481 6.64672566441613 652.204021692691 43.9080276085912 89.1105154235955 897513.402850357 T 6 CATAB v2.0e-lin.ifort 2019-May-30 09:27:12 2019-May-30 09:27
2162-Mar-15 19:57 00:10 Jupiter 1.77373094867847 1.77372915550016 1.77373274192373 2.65037997269372 2.46362326543472 2510788.331312993 10.0802865462468 701.406651413212 72.7349367394189 -78.7300357749111 815201.815056258 T 6 CATAB v2.0e-lin.ifort 2019-May-30 09:27:12 2019-May-30 09:27
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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