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351545 (2005 TE15)
Classification: Apollo [NEO]          SPK-ID: 2351545
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 62 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3436238714626104 4.4118e-08  
a 1.204320100479642 3.6359e-09 au
q .7904869650725872 5.4376e-08 au
i 13.1287219794281 6.4017e-06 deg
node 10.90042444040775 1.582e-05 deg
peri 241.178832171041 2.0742e-05 deg
M 162.7077290458676 2.4833e-05 deg
tp 2458382.318957748532
(2018-Sep-20.81895775)
3.2578e-05 TDB
period 482.7378248785376
1.32
2.1861e-06
5.985e-09
d
yr
n .745746410260228 3.3772e-09 deg/d
Q 1.618153235886696 4.8853e-09 au
  Orbit Determination Parameters
   # obs. used (total)      228  
   data-arc span      4423 days (12.11 yr)  
   first obs. used      2005-10-04  
   last obs. used      2017-11-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52251  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Nov-13 06:21:55  

Additional Information
 Earth MOID = .0547884 au 
 Jupiter MOID = 3.46174 au 
 T_jup = 5.201 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456568.5 (2013-Oct-03.0) TDB
Reference: JPL 62 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3437076755568123 4.4111e-08  
q .7903724694630847 5.4366e-08 au
tp 2456451.484222880791
(2013-Jun-07.98422288)
2.6163e-05 TDB
node 10.93381123400098 1.582e-05 deg
peri 241.1784028502399 2.0723e-05 deg
i 13.13040562310702 6.4016e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      228  
   data-arc span      4423 days (12.11 yr)  
   first obs. used      2005-10-04  
   last obs. used      2017-11-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52251  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Nov-13 06:21:55  

Additional Information
 Jupiter MOID = 3.46174 au 
 T_jup = 5.201 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.94581052138496E-15 -2.395972517470196E-15 1.043772080512281E-14 -1.773936598007344E-16 -3.275375788954097E-14 4.450103970316114E-14
q -2.395972517470196E-15 2.955712775965268E-15 2.988774290663646E-14 3.622801841451724E-15 5.967675639210716E-14 -4.932120035793292E-14
tp 1.043772080512281E-14 2.988774290663646E-14 6.844898640869493E-10 2.431036257189234E-11 3.530579080913214E-10 6.927815721066568E-11
node -1.773936598007344E-16 3.622801841451724E-15 2.431036257189234E-11 2.502698627349902E-10 -2.300189168351156E-10 -1.451107621064257E-11
peri -3.275375788954097E-14 5.967675639210716E-14 3.530579080913214E-10 -2.300189168351156E-10 4.294418440258843E-10 4.969401917621374E-11
i 4.450103970316114E-14 -4.932120035793292E-14 6.927815721066568E-11 -1.451107621064257E-11 4.969401917621374E-11 4.098022956615047E-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 19.7   n/a MPO264878  

351545 (2005 TE15)          Discovered 2005-Oct-04 by NEAT at Palomar
Reference: 20130127/Numbers.arcLast Updated: 2013-01-31

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