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15637 (2000 JY53)
Classification: Main-belt Asteroid          SPK-ID: 2015637
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07945162248858247 5.4412e-08  
a 3.172424338824542 2.1123e-08 au
q 2.920370077882663 1.7237e-07 au
i 15.37688242432979 5.8877e-06 deg
node 238.1623640575708 1.6556e-05 deg
peri 328.301466725408 3.0769e-05 deg
M 192.7767474207847 2.8298e-05 deg
tp 2459959.192880544002
(2023-Jan-14.69288054)
0.00016596 TDB
period 2063.884248587677
5.65
2.0613e-05
5.644e-08
d
yr
n .1744283867888179 1.7421e-09 deg/d
Q 3.42447859976642 2.2802e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1816  
   data-arc span      14625 days (40.04 yr)  
   first obs. used      1980-11-01  
   last obs. used      2020-11-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .46677  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 03:00:35  

Additional Information
 Earth MOID = 1.9238 au 
 Jupiter MOID = 1.61472 au 
 T_jup = 3.141 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456982.5 (2014-Nov-21.0) TDB
Reference: JPL 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08004726755244253 5.4364e-08  
q 2.917973605123638 1.724e-07 au
tp 2457905.514536503316
(2017-Jun-01.01453650)
0.00015721 TDB
node 238.2450951705072 1.6595e-05 deg
peri 330.107887517907 3.0601e-05 deg
i 15.35937400760159 5.8836e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1816  
   data-arc span      14625 days (40.04 yr)  
   first obs. used      1980-11-01  
   last obs. used      2020-11-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .46677  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 03:00:35  

Additional Information
 Jupiter MOID = 1.61472 au 
 T_jup = 3.141 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.955470482837803E-15 -9.312604863806888E-15 3.976721323342589E-13 -3.884892290526164E-15 6.657930833976376E-14 2.3890787923049E-15
q -9.312604863806888E-15 2.972119505309682E-14 -4.029456824494379E-13 1.201742350274749E-14 -9.984753815384387E-14 -6.417402122153391E-15
tp 3.976721323342589E-13 -4.029456824494379E-13 2.471386604051629E-8 -1.512450327639435E-12 4.06173462333969E-9 -6.422832063958111E-12
node -3.884892290526164E-15 1.201742350274749E-14 -1.512450327639435E-12 2.753902517029359E-10 -2.65441509455935E-10 -3.748256005282746E-11
peri 6.657930833976376E-14 -9.984753815384387E-14 4.06173462333969E-9 -2.65441509455935E-10 9.363952765731972E-10 3.485762454747751E-11
i 2.3890787923049E-15 -6.417402122153391E-15 -6.422832063958111E-12 -3.748256005282746E-11 3.485762454747751E-11 3.461717598725538E-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 12.7   n/a MPO332964  
diameter diameter 17.582 km 0.189 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.067   0.002 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

15637 (2000 JY53)          Discovered 2000-May-06 by LINEAR at Socorro
Reference: 20000621/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 2000 JY53 = 1980 VF3 = 1999 BV22 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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