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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 
[ 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 27.6   n/a MPO290419  

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