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(2013 TX68)
Classification: Apollo [NEO]          SPK-ID: 3648983
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


Orbital Elements at Epoch 2456570.5 (2013-Oct-05.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .551674919747994 0.0012399  
a 1.660230620033532 0.0037412 au
q .7443230259633711 0.00038131 au
i 1.110357782027461 0.0028694 deg
node 165.7451582627636 0.013342 deg
peri 286.9729813613895 0.012007 deg
M 334.3782550617863 0.10314 deg
tp 2456626.110558752872
(2013-Nov-29.61055875)
0.035893 TDB
period 781.3597863576896
2.14
2.6411
0.007231
d
yr
n .4607352544698273 0.0015574 deg/d
Q 2.576138214103694 0.0058052 au
  Orbit Determination Parameters
   # obs. used (total)      36  
   data-arc span      10 days  
   first obs. used      2013-09-29  
   last obs. used      2013-10-09  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .43976  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 08:45:18  

Additional Information
 Earth MOID = 1.79804E-5 au 
 Jupiter MOID = 2.65978 au 
 T_jup = 4.076 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 1.537462970881467E-6 -4.728029747204507E-7 -4.450557021689341E-5 1.646541230405669E-5 -1.481499567457474E-5 3.556987185257591E-6
q -4.728029747204507E-7 1.453975762897068E-7 1.368636284424613E-5 -5.063931261407164E-6 4.556290537043294E-6 -1.093874750536613E-6
tp -4.450557021689341E-5 1.368636284424613E-5 .001288332316910321 -.0004765136786075153 .0004287543997693553 -.0001029593442825172
node 1.646541230405669E-5 -5.063931261407164E-6 -.0004765136786075153 .0001780199020159766 -.0001601949853223427 3.81768960634769E-5
peri -1.481499567457474E-5 4.556290537043294E-6 .0004287543997693553 -.0001601949853223427 .0001441664718466345 -3.435063589106107E-5
i 3.556987185257591E-6 -1.093874750536613E-6 -.0001029593442825172 3.81768960634769E-5 -3.435063589106107E-5 8.233458968581676E-6

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 25.2   n/a MPO369196  

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