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(2013 TS5)
Classification: Apollo [NEO]          SPK-ID: 3648863
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4881512138476434 3.1886e-07  
a 1.108411663914407 5.9758e-09 au
q .5673391647317032 3.5417e-07 au
i 54.30730850556274 4.2337e-05 deg
node 195.5787937185543 8.9816e-06 deg
peri 336.3286330357047 2.1685e-05 deg
M 155.164069858384 6.3216e-05 deg
tp 2458816.787494858543
(2019-Nov-29.28749486)		 7.4425e-05 TDB
period 426.2359314968099
1.17		 3.447e-06
9.437e-09		 d
yr
n .8446026564109467 6.8303e-09 deg/d
Q 1.649484163097111 8.8929e-09 au
   Orbit Determination Parameters
   # obs. used (total)      121  
   data-arc span      2566 days (7.03 yr)  
   first obs. used      2013-10-03  
   last obs. used      2020-10-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5135  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-13 07:02:34  

Additional Information
 Earth MOID = .413948 au 
 Jupiter MOID = 3.38067 au 
 T_jup = 5.164 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458084.5 (2017-Nov-27.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4882490072074357 3.1888e-07  
q .5672210406344375 3.5411e-07 au
tp 2457964.323491399945
(2017-Jul-29.82349140)		 7.2939e-05 TDB
node 195.5826650063443 8.9762e-06 deg
peri 336.3292402963352 2.1675e-05 deg
i 54.31116115527777 4.2341e-05 deg
   Orbit Determination Parameters
   # obs. used (total)      121  
   data-arc span      2566 days (7.03 yr)  
   first obs. used      2013-10-03  
   last obs. used      2020-10-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5135  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-13 07:02:34  

Additional Information
 Jupiter MOID = 3.38067 au 
 T_jup = 5.164 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.016859257888648E-13 -1.129163266831491E-13 -1.955178530252821E-11 -2.320021017851551E-13 -2.463828700451422E-12 -8.187000268747984E-13
q -1.129163266831491E-13 1.253958448065504E-13 2.170755523350537E-11 2.596541897092026E-13 2.735233250417698E-12 9.165620987357262E-13
tp -1.955178530252821E-11 2.170755523350537E-11 5.320158963280697E-9 9.771038826716183E-11 1.228976070185009E-9 4.25402543527942E-11
node -2.320021017851551E-13 2.596541897092026E-13 9.771038826716183E-11 8.057250026599749E-11 -8.5425159606002E-12 2.758649524723291E-10
peri -2.463828700451422E-12 2.735233250417698E-12 1.228976070185009E-9 -8.5425159606002E-12 4.698120095413323E-10 -1.864990480727E-10
i -8.187000268747984E-13 9.165620987357262E-13 4.25402543527942E-11 2.758649524723291E-10 -1.864990480727E-10 1.79280161488187E-9

[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 19.2   n/a E2014V42  

[ show close-approach data ]
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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