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59684 (1999 JB107)
Classification: Main-belt Asteroid          SPK-ID: 2059684
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07424470193525552 5.5621e-08  
a 2.543647219667678 1.1382e-08 au
q 2.35479489001501 1.4487e-07 au
i 7.962560047772394 5.494e-06 deg
node 210.7350247701154 2.5198e-05 deg
peri 115.7351613175409 4.5623e-05 deg
M 344.898301114067 3.5797e-05 deg
tp 2459062.659433883312
(2020-Aug-01.15943388)
0.00014732 TDB
period 1481.780054483574
4.06
9.9455e-06
2.723e-08
d
yr
n .2429510364312916 1.6307e-09 deg/d
Q 2.732499549320346 1.2227e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1038  
   data-arc span      7754 days (21.23 yr)  
   first obs. used      1999-05-10  
   last obs. used      2020-08-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52908  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 05:23:03  

Additional Information
 Earth MOID = 1.35714 au 
 Jupiter MOID = 2.49144 au 
 T_jup = 3.427 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457174.5 (2015-Jun-01.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07417101825176461 5.624e-08  
q 2.353879693096744 1.465e-07 au
tp 2457585.939803809329
(2016-Jul-16.43980381)
0.00014667 TDB
node 210.7958310201368 2.5175e-05 deg
peri 116.8234548013775 4.5215e-05 deg
i 7.967236292439251 5.4969e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1038  
   data-arc span      7754 days (21.23 yr)  
   first obs. used      1999-05-10  
   last obs. used      2020-08-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52908  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 05:23:03  

Additional Information
 Jupiter MOID = 2.49144 au 
 T_jup = 3.427 
Orbit Covariance (6×6)
  e q tp node peri i
e 3.16294721057383E-15 -8.220018725470438E-15 5.439988244307269E-12 -8.66515829727372E-15 1.483485860133902E-12 -9.658168160380581E-15
q -8.220018725470438E-15 2.146130560752186E-14 -1.4060508688697E-11 2.2410451653629E-14 -3.844536073039254E-12 2.540026113234781E-14
tp 5.439988244307269E-12 -1.4060508688697E-11 2.151319729028543E-8 -8.47660122285335E-12 5.507409941257543E-9 -2.577113275121141E-11
node -8.66515829727372E-15 2.2410451653629E-14 -8.47660122285335E-12 6.337606976240228E-10 -6.298685568956917E-10 -4.490000122421421E-11
peri 1.483485860133902E-12 -3.844536073039254E-12 5.507409941257543E-9 -6.298685568956917E-10 2.044354578525662E-9 3.78752330622057E-11
i -9.658168160380581E-15 2.540026113234781E-14 -2.577113275121141E-11 -4.490000122421421E-11 3.78752330622057E-11 3.021581074363614E-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 15.0   n/a MPO287188  
diameter diameter 4.618 km 0.224 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.100   0.025 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

59684 (1999 JB107)          Discovered 1999-May-13 by LINEAR at Socorro
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 1999 JB107 = 2000 RN59 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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