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(2014 TM)
Classification: Apollo [NEO]          SPK-ID: 3692290
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .232254295411127 0.00040618  
a 1.251311852092019 0.00061978 au
q .9606892995447948 3.2496e-05 au
i 9.735008194213073 0.013038 deg
node 9.453508906392587 0.00028065 deg
peri 42.91770312708825 0.012218 deg
M 348.1261455776846 1.0508 deg
tp 2459017.363044391405
(2020-Jun-16.86304439)
1.5049 TDB
period 511.2658253158783
1.40
0.37985
0.00104
d
yr
n .7041346833177812 0.00052314 deg/d
Q 1.541934404639244 0.00076373 au
  Orbit Determination Parameters
   # obs. used (total)      24  
   data-arc span      1 day  
   first obs. used      2014-10-02  
   last obs. used      2014-10-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .55186  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:38:17  

Additional Information
 Earth MOID = .00957687 au 
 Jupiter MOID = 3.81452 au 
 T_jup = 5.099 
[ 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 26.2   n/a MPO309138  

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