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59607 (1999 JV65)
Classification: Main-belt Asteroid          SPK-ID: 2059607
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .02821533499960056 2.7012e-08  
a 2.419072274816052 8.0723e-09 au
q 2.350817340193871 6.4758e-08 au
i 3.141117575366894 4.0838e-06 deg
node 196.6098690840141 5.3104e-05 deg
peri 106.6059706850645 9.3307e-05 deg
M 130.3508004665567 7.5629e-05 deg
tp 2458502.897109353863
(2019-Jan-19.39710935)		 0.00028913 TDB
period 1374.268819151358
3.76		 6.8788e-06
1.883e-08		 d
yr
n .2619574823958447 1.3112e-09 deg/d
Q 2.487327209438233 8.3e-09 au
   Orbit Determination Parameters
   # obs. used (total)      1816  
   data-arc span      10569 days (28.94 yr)  
   first obs. used      1991-02-19  
   last obs. used      2020-01-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .4966  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 12:50:34  

Additional Information
 Earth MOID = 1.33787 au 
 Jupiter MOID = 2.55134 au 
 T_jup = 3.512 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456977.5 (2014-Nov-16.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .02912401235441363 2.7075e-08  
q 2.348437805188551 6.5059e-08 au
tp 2457132.068889551761
(2015-Apr-19.56888955)		 0.00028117 TDB
node 196.634708519672 5.3083e-05 deg
peri 107.4896603407632 9.1331e-05 deg
i 3.141108046199289 4.0856e-06 deg
   Orbit Determination Parameters
   # obs. used (total)      1816  
   data-arc span      10569 days (28.94 yr)  
   first obs. used      1991-02-19  
   last obs. used      2020-01-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .4966  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 12:50:34  

Additional Information
 Jupiter MOID = 2.55134 au 
 T_jup = 3.512 
Orbit Covariance (6×6)
  e q tp node peri i
e 7.330567672025909E-16 -1.748746396086716E-15 1.199246877919936E-12 -9.110008014618747E-16 3.051395053260017E-13 9.113581539467643E-17
q -1.748746396086716E-15 4.232661679820418E-15 -3.358837902908331E-12 1.963561460469356E-15 -8.608864758761417E-13 -8.355270938699619E-17
tp 1.199246877919936E-12 -3.358837902908331E-12 7.905419929965275E-8 -3.940340337150188E-11 2.090250910743987E-8 4.948951609849102E-13
node -9.110008014618747E-16 1.963561460469356E-15 -3.940340337150188E-11 2.817812891734346E-9 -2.823544986229315E-9 1.043743790346838E-11
peri 3.051395053260017E-13 -8.608864758761417E-13 2.090250910743987E-8 -2.823544986229315E-9 8.341420669930109E-9 -1.029854697946141E-11
i 9.113581539467643E-17 -8.355270938699619E-17 4.948951609849102E-13 1.043743790346838E-11 -1.029854697946141E-11 1.66921289010296E-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 14.4   n/a MPO452977  
diameter diameter 4.008 km 0.082 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.159   0.044 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

59607 (1999 JV65)          Discovered 1999-May-12 by LINEAR at Socorro
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 1999 JV65 = 2000 QM91 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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