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351058 (2003 SH296)
Classification: Main-belt Asteroid          SPK-ID: 2351058
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .215401246458218 1.3676e-07  
a 2.64363206218825 2.5334e-08 au
q 2.074190420815992 3.5549e-07 au
i 10.86638401341557 8.8009e-06 deg
node 323.8606250578482 9.259e-05 deg
peri 58.0587751947466 9.9217e-05 deg
M 313.8119547138463 3.1533e-05 deg
tp 2459201.931332024597
(2020-Dec-18.43133202)
0.0001389 TDB
period 1570.001048530921
4.30
2.2568e-05
6.179e-08
d
yr
n .2292992099189097 3.296e-09 deg/d
Q 3.213073703560509 3.0791e-08 au
  Orbit Determination Parameters
   # obs. used (total)      67  
   data-arc span      5722 days (15.67 yr)  
   first obs. used      2003-09-29  
   last obs. used      2019-05-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56952  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-24 06:36:48  

Additional Information
 Earth MOID = 1.09878 au 
 Jupiter MOID = 2.36352 au 
 T_jup = 3.335 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456710.5 (2014-Feb-22.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2181677762639629 1.3726e-07  
q 2.06469878740366 3.5831e-07 au
tp 2456065.653451099933
(2012-May-18.15345110)
0.00012141 TDB
node 324.0298312554262 9.2754e-05 deg
peri 58.11837723017882 9.9086e-05 deg
i 10.86284185996662 8.8e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      67  
   data-arc span      5722 days (15.67 yr)  
   first obs. used      2003-09-29  
   last obs. used      2019-05-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56952  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-24 06:36:48  

Additional Information
 Jupiter MOID = 2.36352 au 
 T_jup = 3.335 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.883943176416953E-14 -4.911752919045631E-14 4.879958591697456E-12 4.279840259151438E-13 3.836815249435498E-13 -1.430796425183096E-13
q -4.911752919045631E-14 1.283881939267838E-13 -1.255965927319843E-11 -1.106995214660833E-12 -9.216513113111986E-13 3.752519796871924E-13
tp 4.879958591697456E-12 -1.255965927319843E-11 1.473996590470496E-8 -1.154474847652901E-10 4.549830413386005E-9 -8.385214351765914E-11
node 4.279840259151438E-13 -1.106995214660833E-12 -1.154474847652901E-10 8.603327585068215E-9 -8.496610983641678E-9 5.219901124549838E-11
peri 3.836815249435498E-13 -9.216513113111986E-13 4.549830413386005E-9 -8.496610983641678E-9 9.817940945117855E-9 -7.129880708592975E-11
i -1.430796425183096E-13 3.752519796871924E-13 -8.385214351765914E-11 5.219901124549838E-11 -7.129880708592975E-11 7.744020521366476E-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 17.3   n/a MPO476630  

351058 (2003 SH296)          Discovered 2003-Sep-29 by LONEOS at Anderson Mesa
Reference: 20130127/Numbers.arcLast Updated: 2013-01-31

[ 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
2035-Jun-18 11:15 00:02 Thisb 0.00965209559519838 0.00964165579834587 0.00966253722841991 4.49518373774276 4.4951835805959 2464496.968677991 1.90417811670315 566.157050102979 175.947185445291 24.4775970047105 4114.69587063733 T 6 CATAB v2.0f-lin.ifort 2019-Sep-24 06:36:49 2019-Sep-24 06:36
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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