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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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .02816273930318296 2.6961e-08  
a 2.419332521823392 7.6657e-09 au
q 2.351197490723568 6.4763e-08 au
i 3.141040332032808 3.7938e-06 deg
node 196.6009368845711 5.2731e-05 deg
peri 106.8955831998011 8.7232e-05 deg
M 182.4449046906869 6.9041e-05 deg
tp 2459878.410578751599
(2022-Oct-25.91057875)
0.0002635 TDB
period 1374.490593612241
3.76
6.5327e-06
1.789e-08
d
yr
n .2619152154791392 1.2448e-09 deg/d
Q 2.487467552923216 7.8816e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1994  
   data-arc span      10926 days (29.91 yr)  
   first obs. used      1991-02-19  
   last obs. used      2021-01-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48823  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 05:47:40  

Additional Information
 Earth MOID = 1.33629 au 
 Jupiter MOID = 2.55026 au 
 T_jup = 3.512 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457147.5 (2015-May-05.0) TDB
Reference: JPL 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .02918379510276999 2.6993e-08  
q 2.348487786663035 6.4929e-08 au
tp 2457131.464277467038
(2015-Apr-18.96427747)
0.00025497 TDB
node 196.6288271584729 5.2708e-05 deg
peri 107.3278610017217 8.5333e-05 deg
i 3.141113734076358 3.7956e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1994  
   data-arc span      10926 days (29.91 yr)  
   first obs. used      1991-02-19  
   last obs. used      2021-01-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48823  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 05:47:40  

Additional Information
 Jupiter MOID = 2.55026 au 
 T_jup = 3.512 
Orbit Covariance (6×6)
  e q tp node peri i
e 7.286076205705451E-16 -1.74122122742901E-15 1.348680176114918E-12 -3.456980365202349E-16 3.44744727126907E-13 2.169917223953954E-16
q -1.74122122742901E-15 4.215722207794941E-15 -3.415590829680415E-12 4.003894506736691E-16 -8.745716911001857E-13 -4.293929780275963E-16
tp 1.348680176114918E-12 -3.415590829680415E-12 6.501026022124465E-8 -3.28001062080291E-11 1.711737186598573E-8 2.348115004502086E-12
node -3.456980365202349E-16 4.003894506736691E-16 -3.28001062080291E-11 2.778108410726839E-9 -2.782147306881095E-9 2.145590339149402E-12
peri 3.44744727126907E-13 -8.745716911001857E-13 1.711737186598573E-8 -2.782147306881095E-9 7.281728811273558E-9 -1.525240343186557E-12
i 2.169917223953954E-16 -4.293929780275963E-16 2.348115004502086E-12 2.145590339149402E-12 -1.525240343186557E-12 1.44069462650362E-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 14.42   n/a E2021B10  
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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