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(2015 FT33)
Classification: Apollo [NEO]          SPK-ID: 3713936
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 2457100.5 (2015-Mar-19.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3932695274113909 0.0010198  
a 1.663668463050406 0.0028173 au
q 1.009398352817338 1.5557e-05 au
i 4.962750626691077 0.013192 deg
node 327.6813763416368 0.0062865 deg
peri 256.8603845455301 0.003696 deg
M 338.1737936912583 0.052167 deg
tp 2457148.019773092610
(2015-May-05.51977309)
0.0074267 TDB
period 783.7879873099145
2.15
1.9909
0.005451
d
yr
n .4593078815045092 0.0011667 deg/d
Q 2.317938573283475 0.0039252 au
  Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      10 days  
   first obs. used      2015-03-18  
   last obs. used      2015-03-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .479  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:35:01  

Additional Information
 Earth MOID = .0772117 au 
 Jupiter MOID = 2.68437 au 
 T_jup = 4.164 
[ 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 24.3   n/a MPO332797  

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