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(2014 FT37)
Classification: Apollo [NEO]          SPK-ID: 3666679
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .436784747426705 0.00015998  
a 1.7409250933122 0.00048361 au
q .9805155661410178 6.1419e-06 au
i 3.788363234782196 0.0012875 deg
node 7.26164032082328 0.00011656 deg
peri 202.3496264114638 0.00011375 deg
M 239.8174182606145 0.40023 deg
tp 2459280.596436148286
(2021-Mar-07.09643615)
1.0495 TDB
period 839.0127384019911
2.30
0.34961
0.0009572
d
yr
n .4290757261751077 0.00017879 deg/d
Q 2.501334620483382 0.00069485 au
  Orbit Determination Parameters
   # obs. used (total)      71  
   data-arc span      3 days  
   first obs. used      2014-03-25  
   last obs. used      2014-03-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .28586  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:41:53  

Additional Information
 Earth MOID = .00232856 au 
 Jupiter MOID = 2.46691 au 
 T_jup = 4.027 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456743.5 (2014-Mar-27.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4424811740194287 0.00015626  
q .9826736059683735 5.9622e-06 au
tp 2456762.638288022572
(2014-Apr-15.13828802)
6.3351e-05 TDB
node 7.46885241968827 6.1714e-05 deg
peri 200.9996152774901 0.0012655 deg
i 4.08527580057866 0.0010843 deg
  Orbit Determination Parameters
   # obs. used (total)      71  
   data-arc span      3 days  
   first obs. used      2014-03-25  
   last obs. used      2014-03-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .28586  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:41:53  

Additional Information
 Jupiter MOID = 2.46691 au 
 T_jup = 4.027 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.441829840728183E-8 -9.311854583866278E-10 4.383324697178018E-9 -9.614720683456584E-9 1.974334681273003E-7 1.694208452513958E-7
q -9.311854583866278E-10 3.554785297812019E-11 -1.779387140422313E-10 3.661458256131538E-10 -7.542690693193031E-9 -6.458472118208346E-9
tp 4.383324697178018E-9 -1.779387140422313E-10 4.013305698649041E-9 -1.586690439443414E-9 3.950241159412783E-8 2.97988412397463E-8
node -9.614720683456584E-9 3.661458256131538E-10 -1.586690439443414E-9 3.808665745602336E-9 -7.757837339211787E-8 -6.676321650165982E-8
peri 1.974334681273003E-7 -7.542690693193031E-9 3.950241159412783E-8 -7.757837339211787E-8 1.601472105318285E-6 1.369081746980733E-6
i 1.694208452513958E-7 -6.458472118208346E-9 2.97988412397463E-8 -6.676321650165982E-8 1.369081746980733E-6 1.175782841877E-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 27.6   n/a MPO290419  

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