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97373 (2000 AE63)
Classification: Main-belt Asteroid          SPK-ID: 2097373
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2251015940760158 4.3367e-08  
a 2.969165338415578 1.7429e-08 au
q 2.300801487662978 1.3056e-07 au
i 9.607271817623536 4.7017e-06 deg
node 330.771164818561 3.0212e-05 deg
peri 104.5508537345195 3.2591e-05 deg
M 62.6573491662605 1.0647e-05 deg
tp 2458875.248343982029
(2020-Jan-26.74834398)
5.5093e-05 TDB
period 1868.744811654433
5.12
1.6455e-05
4.505e-08
d
yr
n .1926426753159976 1.6962e-09 deg/d
Q 3.637529189168177 2.1353e-08 au
  Orbit Determination Parameters
   # obs. used (total)      818  
   data-arc span      8226 days (22.52 yr)  
   first obs. used      1998-09-14  
   last obs. used      2021-03-23  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .48049  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 08:26:39  

Additional Information
 Earth MOID = 1.33804 au 
 Jupiter MOID = 1.75014 au 
 T_jup = 3.204 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457737.5 (2016-Dec-15.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2240351819391316 4.3184e-08  
q 2.304219465321593 1.2973e-07 au
tp 2457008.036728746672
(2014-Dec-16.53672875)
5.7819e-05 TDB
node 330.8168357376304 3.0208e-05 deg
peri 104.7125154165814 3.2626e-05 deg
i 9.605958082330375 4.7022e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      818  
   data-arc span      8226 days (22.52 yr)  
   first obs. used      1998-09-14  
   last obs. used      2021-03-23  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .48049  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 08:26:39  

Additional Information
 Jupiter MOID = 1.75014 au 
 T_jup = 3.204 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.864874029027423E-15 -5.571514279299625E-15 -9.1805612353704E-13 -1.579532075263479E-14 -2.177180701156232E-13 -1.016416832829102E-14
q -5.571514279299625E-15 1.682901233690503E-14 2.49314948172249E-12 5.218374479991449E-14 6.100161920846225E-13 3.220280740839769E-14
tp -9.1805612353704E-13 2.49314948172249E-12 3.34299925825065E-9 1.026238224796484E-11 7.436064619303661E-10 5.193169662115117E-12
node -1.579532075263479E-14 5.218374479991449E-14 1.026238224796484E-11 9.125390473809348E-10 -8.962714101862914E-10 3.956297937945233E-11
peri -2.177180701156232E-13 6.100161920846225E-13 7.436064619303661E-10 -8.962714101862914E-10 1.064484474983407E-9 -3.733352189991699E-11
i -1.016416832829102E-14 3.220280740839769E-14 5.193169662115117E-12 3.956297937945233E-11 -3.733352189991699E-11 2.211077172103661E-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 14.99   n/a MPCxxxxx  
diameter diameter 2.586 km 0.622 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.382   0.219 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

97373 (2000 AE63)          Discovered 2000-Jan-04 by LINEAR at Socorro
Reference: 20050224/Numbers.arcLast Updated: 2005-02-28

[ 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
1926-Apr-23 21:22 00:02 Jupiter 1.88608026015636 1.88607915275575 1.88608136755739 3.52003578451506 3.39005442912838 2424629.390070529 2.29420335897804 125.288139973151 37.1588739619419 79.2616252389571 1351743.68525554 T 25 CATAB v2.0g-lin.ifort 2021-May-04 08:26:43 2021-May-04 08:26
2007-Mar-04 00:21 < 00:01 Jupiter 1.90582187700128 1.90582119174374 1.90582256225958 1.25873622843715 0.833989151186078 2454163.514650834 0.462810946633403 348.270433986695 203.698508645235 5.68815747572576 1479642.5725234 T 25 CATAB v2.0g-lin.ifort 2021-May-04 08:26:43 2021-May-04 08:26
2043-Apr-30 20:35 < 00:01 Jupiter 1.80712649454861 1.80712586047339 1.80712712862414 1.73047607464391 1.43426731791723 2467370.357983720 0.852978547414278 171.48031537779 60.4501975000954 55.7103229214306 2021659.13847423 T 25 CATAB v2.0g-lin.ifort 2021-May-04 08:26:43 2021-May-04 08:26
2079-Jun-05 16:17 00:02 Jupiter 1.74843476461409 1.74843424000101 1.74843528922967 2.30012685812768 2.0788677782843 2480555.178170194 1.82891418058904 229.667686154564 18.2876203722103 77.1874213860369 2048621.58775322 T 25 CATAB v2.0g-lin.ifort 2021-May-04 08:26:43 2021-May-04 08:26
2115-Jul-01 12:22 00:03 Jupiter 1.7543247963476 1.75432414803137 1.75432544466463 2.81783697163454 2.64094033782713 2493729.015431254 2.90139475444186 235.72884252251 14.9607726911599 86.7433375950978 1625640.63458079 T 25 CATAB v2.0g-lin.ifort 2021-May-04 08:26:43 2021-May-04 08:26
2151-Jul-30 12:18 00:04 Jupiter 1.81144556013751 1.81144382462055 1.8114472956555 3.30189950039285 3.15711113604663 2506907.012368627 4.11837520427621 179.427156366371 50.7508763156509 76.7097340018038 910650.584996224 T 25 CATAB v2.0g-lin.ifort 2021-May-04 08:26:43 2021-May-04 08:26
2187-Sep-06 11:59 00:05 Jupiter 1.93463827625926 1.93463513305995 1.93464141948871 3.81535906270598 3.69882760128448 2520093.998970452 5.29874863706912 431.585764937883 35.0673101981768 72.028608147368 1833545.96533599 T 25 CATAB v2.0g-lin.ifort 2021-May-04 08:26:43 2021-May-04 08:26

Alternate Designations
 2000 AE63 = 1998 RK36 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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