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(2012 TE79)
Classification: Apollo [NEO]          SPK-ID: 3610174
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 2456210.5 (2012-Oct-10.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4480193422054222 0.0010162  
a 1.623210151793505 0.0027137 au
q .8959806073258154 0.00015163 au
i 3.280183119154446 0.006439 deg
node 13.68378174027985 0.00055086 deg
peri 60.25857833613021 0.00081978 deg
M 338.3025717237454 0.063373 deg
tp 2456256.026714796420
(2012-Nov-24.52671480)
0.018804 TDB
period 755.3714254996676
2.07
1.8943
0.005186
d
yr
n .4765867331582805 0.0011952 deg/d
Q 2.350439696261195 0.0039296 au
  Orbit Determination Parameters
   # obs. used (total)      28  
   data-arc span      5 days  
   first obs. used      2012-10-09  
   last obs. used      2012-10-14  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .39078  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 06:46:19  

Additional Information
 Earth MOID = .0122924 au 
 Jupiter MOID = 2.96752 au 
 T_jup = 4.203 
[ 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 26.6   n/a MPO240141  

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