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160783 (2000 SB292)
Classification: Main-belt Asteroid          SPK-ID: 2160783
[ 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 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09488481485001657 4.6412e-08  
a 2.373219195334981 1.729e-08 au
q 2.148036731387116 1.086e-07 au
i 4.820417356424134 5.0539e-06 deg
node 247.5908366522789 6.8895e-05 deg
peri 28.57221740426217 7.6251e-05 deg
M 270.5921590137343 3.3711e-05 deg
tp 2459532.148710001076
(2021-Nov-13.64871000)		 0.00012526 TDB
period 1335.381039105149
3.66		 1.4593e-05
3.995e-08		 d
yr
n .2695859754315812 2.9461e-09 deg/d
Q 2.598401659282846 1.893e-08 au
   Orbit Determination Parameters
   # obs. used (total)      351  
   data-arc span      7089 days (19.41 yr)  
   first obs. used      2000-09-03  
   last obs. used      2020-01-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .63618  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 13:25:00  

Additional Information
 Earth MOID = 1.13132 au 
 Jupiter MOID = 2.48073 au 
 T_jup = 3.532 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456939.5 (2014-Oct-09.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09553631332776427 4.6347e-08  
q 2.146621831541862 1.0859e-07 au
tp 2456861.575655055788
(2014-Jul-23.07565506)		 0.00012583 TDB
node 247.6533489274558 6.8956e-05 deg
peri 28.62736965639317 7.6236e-05 deg
i 4.81791278684986 5.0522e-06 deg
   Orbit Determination Parameters
   # obs. used (total)      351  
   data-arc span      7089 days (19.41 yr)  
   first obs. used      2000-09-03  
   last obs. used      2020-01-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .63618  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 13:25:00  

Additional Information
 Jupiter MOID = 2.48073 au 
 T_jup = 3.532 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.148010127264077E-15 -4.982023478697499E-15 8.41486047403982E-13 2.41277952331446E-15 1.754462097644918E-13 -1.758814232541168E-16
q -4.982023478697499E-15 1.1790862710103E-14 -2.31216805446092E-12 -4.580967438805637E-15 -4.999132504830299E-13 6.734475517786659E-16
tp 8.41486047403982E-13 -2.31216805446092E-12 1.583313200687933E-8 3.736192135196719E-11 4.125567393150113E-9 -3.283945573312566E-12
node 2.41277952331446E-15 -4.580967438805637E-15 3.736192135196719E-11 4.754873867558619E-9 -4.727943769818625E-9 -1.950537307820548E-11
peri 1.754462097644918E-13 -4.999132504830299E-13 4.125567393150113E-9 -4.727943769818625E-9 5.811851654883305E-9 1.860543864649809E-11
i -1.758814232541168E-16 6.734475517786659E-16 -3.283945573312566E-12 -1.950537307820548E-11 1.860543864649809E-11 2.552463377726085E-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 16.4   n/a MPO449863  

160783 (2000 SB292)          Discovered 2000-Sep-27 by LINEAR at Socorro
Reference: 20070828/Numbers.arcLast Updated: 2007-08-30

[ 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
2093-Oct-14 23:32 < 00:01 Juno 0.0206986907694469 0.0206796761070278 0.0207177367044955 7.49301022519879 7.49301014675713 2485800.480689825 0.540019277778346 1585.96155739317 60.6448018595661 -53.3167407388815 40950.3387313073 T 11 CATAB v2.0f-lin.ifort 2020-Feb-24 13:25:14 2020-Feb-24 13:25

Alternate Designations
 2000 SB292 = 2000 TG69 = 2004 UN8 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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