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86302 (1999 VJ46)
Classification: Inner Main-belt Asteroid          SPK-ID: 2086302
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 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07241033676698133 4.8585e-08  
a 1.967983997219642 6.2878e-09 au
q 1.825481613228938 9.3589e-08 au
i 21.41233526140937 5.9513e-06 deg
node 38.12034786161222 9.9522e-06 deg
peri 124.632671675376 4.1783e-05 deg
M 51.73859266910438 3.7481e-05 deg
tp 2458855.575142700180
(2020-Jan-07.07514270)
0.00010511 TDB
period 1008.395202428652
2.76
4.8328e-06
1.323e-08
d
yr
n .357002888483567 1.7109e-09 deg/d
Q 2.110486381210346 6.743e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1026  
   data-arc span      8098 days (22.17 yr)  
   first obs. used      1998-04-22  
   last obs. used      2020-06-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51997  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 20:57:48  

Additional Information
 Earth MOID = .861736 au 
 Jupiter MOID = 2.89439 au 
 T_jup = 3.786 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457361.5 (2015-Dec-05.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07246645308775636 4.8685e-08  
q 1.825568140650768 9.3823e-08 au
tp 2457847.430731157248
(2017-Apr-03.93073116)
0.00010578 TDB
node 38.12872671154899 9.9527e-06 deg
peri 124.7403411005907 4.1668e-05 deg
i 21.41158556067709 5.9514e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1026  
   data-arc span      8098 days (22.17 yr)  
   first obs. used      1998-04-22  
   last obs. used      2020-06-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51997  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 20:57:48  

Additional Information
 Jupiter MOID = 2.89439 au 
 T_jup = 3.786 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.370245800536667E-15 -4.560144893514251E-15 1.912707679311055E-12 3.002187440605814E-15 6.906579998977721E-13 -1.744772710267836E-14
q -4.560144893514251E-15 8.802799129902483E-15 -3.90378581521374E-12 -5.688683367481774E-15 -1.418180814178637E-12 3.323550994910062E-14
tp 1.912707679311055E-12 -3.90378581521374E-12 1.118901541748735E-8 -1.332645815135572E-11 4.284950665806407E-9 7.082216436531774E-12
node 3.002187440605814E-15 -5.688683367481774E-15 -1.332645815135572E-11 9.905648827152792E-11 -9.689085551189184E-11 -1.710015094346232E-11
peri 6.906579998977721E-13 -1.418180814178637E-12 4.284950665806407E-9 -9.689085551189184E-11 1.736188704423491E-9 1.892316405415638E-11
i -1.744772710267836E-14 3.323550994910062E-14 7.082216436531774E-12 -1.710015094346232E-11 1.892316405415638E-11 3.54186765718118E-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 15.8   n/a MPO280336  

86302 (1999 VJ46)          Discovered 1999-Nov-03 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
2079-Sep-15 00:57 < 00:01 Juno 0.034005665980074 0.0339958390358349 0.0340154931650776 11.9690453353107 11.96904530542 2480656.539251274 0.185882488568974 510.415724379106 32.0892564116286 -16.30007982399 45503.0825286104 T 18 CATAB v2.0f-lin.ifort 2020-Nov-12 20:57:50 2020-Nov-12 20:57
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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