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134347 (1992 RV3)
Classification: Main-belt Asteroid          SPK-ID: 2134347
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .185503207608146 7.1469e-08  
a 2.297413158706072 5.6946e-09 au
q 1.871235648564934 1.6308e-07 au
i 3.432429799248931 5.0515e-06 deg
node 320.6809556816027 9.2858e-05 deg
peri 34.39497427585115 9.3219e-05 deg
M 339.6011797927098 9.6557e-06 deg
tp 2459072.570848081653
(2020-Aug-11.07084808)
3.4198e-05 TDB
period 1271.912054017835
3.48
4.729e-06
1.295e-08
d
yr
n .2830384371803053 1.0523e-09 deg/d
Q 2.723590668847212 6.7509e-09 au
  Orbit Determination Parameters
   # obs. used (total)      666  
   data-arc span      10296 days (28.19 yr)  
   first obs. used      1992-09-02  
   last obs. used      2020-11-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49186  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 04:48:16  

Additional Information
 Earth MOID = .867521 au 
 Jupiter MOID = 2.718 au 
 T_jup = 3.568 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457380.5 (2015-Dec-24.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1860191464562731 7.1421e-08  
q 1.869633456260284 1.6306e-07 au
tp 2457801.796300669423
(2017-Feb-17.29630067)
3.2949e-05 TDB
node 320.7380992188004 9.2918e-05 deg
peri 34.62528243562051 9.3276e-05 deg
i 3.431552393951268 5.0525e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      666  
   data-arc span      10296 days (28.19 yr)  
   first obs. used      1992-09-02  
   last obs. used      2020-11-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49186  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 04:48:16  

Additional Information
 Jupiter MOID = 2.718 au 
 T_jup = 3.568 
Orbit Covariance (6×6)
  e q tp node peri i
e 5.100961181812995E-15 -1.16415910644727E-14 1.214695747502218E-12 8.532781869154566E-14 1.717164927892934E-13 -6.384506473712881E-15
q -1.16415910644727E-14 2.658865869843997E-14 -2.767617415686992E-12 -1.951999588838702E-13 -3.922758686876045E-13 1.454836366432772E-14
tp 1.214695747502218E-12 -2.767617415686992E-12 1.085666100458686E-9 2.320917619773034E-11 3.0066904346477E-10 -2.057249106270686E-12
node 8.532781869154566E-14 -1.951999588838702E-13 2.320917619773034E-11 8.633663613223056E-9 -8.61315274193942E-9 3.237693256257048E-10
peri 1.717164927892934E-13 -3.922758686876045E-13 3.0066904346477E-10 -8.61315274193942E-9 8.700368997645568E-9 -3.236915862702204E-10
i -6.384506473712881E-15 1.454836366432772E-14 -2.057249106270686E-12 3.237693256257048E-10 -3.236915862702204E-10 2.552731875225744E-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 16.3   n/a MPO432807  

134347 (1992 RV3)          Discovered 1992-Sep-02 by Elst, E. W. at La Silla
Reference: 20060907/Numbers.arcLast Updated: 2006-09-10

[ 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
1910-Oct-16 02:03 < 00:01 Juno 0.0083518256551023 0.00834444823367316 0.00835920522036612 6.24969368042989 6.24969344734945 2418960.585521451 0.524526658213141 424.90805009044 48.6977206526332 30.2723991251221 13173.1084796211 T 19 CATAB v2.0f-lin.ifort 2020-Dec-18 04:48:19 2020-Dec-18 04:48
2094-Dec-28 11:29 < 00:01 Hebe 0.0297862228650216 0.0297803047838737 0.0297921414955223 5.65240254496095 5.65240250803692 2486239.978644404 0.639822324645783 358.371798774931 38.9363279706171 34.8229173043122 66120.44912438 T 19 CATAB v2.0f-lin.ifort 2020-Dec-18 04:48:19 2020-Dec-18 04:48

Alternate Designations
 1992 RV3 = 1999 RQ96 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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