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79686 (1998 SY58)
Classification: Main-belt Asteroid          SPK-ID: 2079686
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1641743069583791 3.6025e-08  
a 2.325132677971773 7.4939e-09 au
q 1.943405631979477 8.5042e-08 au
i 3.050375083823689 4.0486e-06 deg
node 27.13579790693241 7.0492e-05 deg
peri 314.587246371496 7.1387e-05 deg
M 58.80852751162139 1.14e-05 deg
tp 2458788.952527302990
(2019-Nov-01.45252730)
4.0751e-05 TDB
period 1295.000799941365
3.55
6.2607e-06
1.714e-08
d
yr
n .2779921062722897 1.344e-09 deg/d
Q 2.706859723964069 8.7242e-09 au
  Orbit Determination Parameters
   # obs. used (total)      960  
   data-arc span      8248 days (22.58 yr)  
   first obs. used      1997-04-03  
   last obs. used      2019-11-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54228  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-04 07:38:42  

Additional Information
 Earth MOID = .936777 au 
 Jupiter MOID = 2.68301 au 
 T_jup = 3.555 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456843.5 (2014-Jul-05.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1648419092852656 3.6003e-08  
q 1.941759998675979 8.5065e-08 au
tp 2456199.980423898837
(2012-Sep-29.48042390)
3.9582e-05 TDB
node 27.17423985133459 7.0413e-05 deg
peri 314.7639238101444 7.1302e-05 deg
i 3.05290957561408 4.0505e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      960  
   data-arc span      8248 days (22.58 yr)  
   first obs. used      1997-04-03  
   last obs. used      2019-11-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54228  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-04 07:38:42  

Additional Information
 Jupiter MOID = 2.68301 au 
 T_jup = 3.555 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.296194296308612E-15 -3.054433384240767E-15 3.202126657784022E-14 -2.072822818128227E-15 1.51433905256894E-14 -1.161536122214639E-15
q -3.054433384240767E-15 7.236039605450392E-15 -9.784974362052234E-14 5.236110978381316E-15 -3.767345189555348E-14 2.831761508310873E-15
tp 3.202126657784022E-14 -9.784974362052234E-14 1.566717261221464E-9 5.674418262125142E-12 4.550527773869144E-10 2.10017385791612E-13
node -2.072822818128227E-15 5.236110978381316E-15 5.674418262125142E-12 4.957983221940337E-9 -4.948864946838319E-9 -3.567415062866834E-11
peri 1.51433905256894E-14 -3.767345189555348E-14 4.550527773869144E-10 -4.948864946838319E-9 5.083907489371162E-9 3.570005619998717E-11
i -1.161536122214639E-15 2.831761508310873E-15 2.10017385791612E-13 -3.567415062866834E-11 3.570005619998717E-11 1.640689276195017E-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 15.5   n/a MPO436338  

79686 (1998 SY58)          Discovered 1998-Sep-17 by LONEOS at Anderson Mesa
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

[ show close-approach data ]
Alternate Designations
 1998 SY58 = 1997 GO33 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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