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JPL Small-Body Database Browser
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13202 (1997 FT3)
Classification: Main-belt Asteroid          SPK-ID: 2013202
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1003401511330139 4.6519e-08  
a 2.299311340829112 7.9525e-09 au
q 2.068598093388466 1.0659e-07 au
i 4.521295366432019 4.9285e-06 deg
node 211.7143674369034 4.4013e-05 deg
peri 336.7439325887839 4.7504e-05 deg
M 235.6683201425673 1.9104e-05 deg
tp 2459440.319418138907
(2021-Aug-13.81941814)
6.8476e-05 TDB
period 1273.488709487111
3.49
6.6068e-06
1.809e-08
d
yr
n .2826880186044112 1.4666e-09 deg/d
Q 2.530024588269757 8.7505e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1106  
   data-arc span      10272 days (28.12 yr)  
   first obs. used      1991-09-12  
   last obs. used      2019-10-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59354  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 03:40:58  

Additional Information
 Earth MOID = 1.06968 au 
 Jupiter MOID = 2.43151 au 
 T_jup = 3.582 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.6   n/a MPO431654  

13202 (1997 FT3)          Discovered 1997-Mar-31 by LINEAR at Socorro
Reference: 20000124/Numbers.arcLast Updated: 2004-04-19

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Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2165-Sep-30 17:47 < 00:01 Eunom 0.0483974251756022 0.0483852098412004 0.0484096457308043 6.24066580508639 6.24066575860911 2512083.241246601 0.274992879227803 1000.60197952674 39.5320867729522 -52.5703881416407 145438.364433173 T 21 CATAB v2.0f-lin.ifort 2019-Nov-07 03:41:04 2019-Nov-07 03:41

Alternate Designations
 1997 FT3 = 1995 SO53 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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