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13467 (2676 T-3)
Classification: Main-belt Asteroid          SPK-ID: 2013467
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 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1148165418487867 3.3979e-08  
a 2.325995108019647 7.3609e-09 au
q 2.058932393359636 7.9412e-08 au
i 3.991784125477109 4.1289e-06 deg
node 211.8655878642987 5.1566e-05 deg
peri 39.46041858808395 5.4502e-05 deg
M 122.1237787425363 1.7796e-05 deg
tp 2458560.948916100436
(2019-Mar-18.44891610)
6.3608e-05 TDB
period 1295.721372472796
3.55
6.1507e-06
1.684e-08
d
yr
n .2778375101685361 1.3189e-09 deg/d
Q 2.593057822679658 8.2061e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1442  
   data-arc span      15724 days (43.05 yr)  
   first obs. used      1977-10-07  
   last obs. used      2020-10-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54753  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-13 02:46:11  

Additional Information
 Earth MOID = 1.0467 au 
 Jupiter MOID = 2.42961 au 
 T_jup = 3.562 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456752.5 (2014-Apr-05.0) TDB
Reference: JPL 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1146750748364962 3.4065e-08  
q 2.060459481542511 7.9679e-08 au
tp 2457264.363722717409
(2015-Aug-29.86372272)
6.2782e-05 TDB
node 211.9605555718206 5.156e-05 deg
peri 39.26343033748428 5.4487e-05 deg
i 3.990976330957393 4.1288e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1442  
   data-arc span      15724 days (43.05 yr)  
   first obs. used      1977-10-07  
   last obs. used      2020-10-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54753  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-13 02:46:11  

Additional Information
 Jupiter MOID = 2.42961 au 
 T_jup = 3.562 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.16041364133006E-15 -2.705033305161225E-15 -3.366766873744303E-13 2.91803283781323E-15 -7.910118344039531E-14 -3.893260547945498E-17
q -2.705033305161225E-15 6.348688617357462E-15 8.31997966089115E-13 -5.769794627656989E-15 1.909102378042853E-13 1.087872284168209E-17
tp -3.366766873744303E-13 8.31997966089115E-13 3.941530227517403E-9 -1.27393542440482E-12 1.114779381637275E-9 5.883288694997159E-13
node 2.91803283781323E-15 -5.769794627656989E-15 -1.27393542440482E-12 2.658433756987153E-9 -2.651884900355083E-9 -8.542637140413624E-12
peri -7.910118344039531E-14 1.909102378042853E-13 1.114779381637275E-9 -2.651884900355083E-9 2.968859506962156E-9 8.716260365013863E-12
i -3.893260547945498E-17 1.087872284168209E-17 5.883288694997159E-13 -8.542637140413624E-12 8.716260365013863E-12 1.704716985512461E-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 14.9   n/a MPO492901  

13467 (2676 T-3)          Discovered 1977-Oct-11 by van Houten, C. J., van Houten-Groeneveld, I., Gehrels, T. at Palomar
Reference: 20000124/Numbers.arcLast Updated: 2004-04-19

[ 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
2105-Jun-04 03:03 < 00:01 Amphi 0.0346960229542986 0.0346842609717704 0.0347077853033184 4.7085013276796 4.7085012924903 2490049.627219080 0.402283647239207 612.794303408171 34.600122524408 16.9258096057979 44399.7501532853 T 27 CATAB v2.0f-lin.ifort 2020-Nov-13 02:46:15 2020-Nov-13 02:46
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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