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(2005 TC51)
Classification: Apollo [NEO]          SPK-ID: 3293961
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3057349358671643 0.00097104  
a 1.00736762615578 9.9399e-05 au
q .6993801495783848 0.00090942 au
i 5.669693383840569 0.020214 deg
node 199.1619584449763 0.034859 deg
peri 288.0076368098659 0.038972 deg
M 288.2269657998073 1.9071 deg
tp 2459274.127358066151
(2021-Feb-28.62735807)
1.9672 TDB
period 369.3009387046826
1.01
0.05466
0.0001497
d
yr
n .97481474393944 0.00014428 deg/d
Q 1.315355102733175 0.00012979 au
  Orbit Determination Parameters
   # obs. used (total)      18  
   data-arc span      1 day  
   first obs. used      2005-10-12  
   last obs. used      2005-10-13  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .29551  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 22:56:22  

Additional Information
 Earth MOID = .00301223 au 
 Jupiter MOID = 3.7425 au 
 T_jup = 5.999 
[ show covariance matrix ]

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 27.3   n/a MPO87828  

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