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(2007 FT3)
Classification: Apollo [NEO, PHA]          SPK-ID: 3372217
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 2454180.5 (2007-Mar-21.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3077514365302609 0.0062291  
a 1.129600011655869 0.018589 au
q .7819639853641759 0.0066686 au
i 26.86573107304766 0.42917 deg
node 9.892196653008442 0.17362 deg
peri 277.1896528906445 2.1394 deg
M 297.9457653118639 2.6603 deg
tp 2454256.088265917683
(2007-Jun-04.58826592)
1.3746 TDB
period 438.5160153392142
1.20
10.825
0.02964
d
yr
n .8209506321485701 0.020265 deg/d
Q 1.477236037947562 0.02431 au
  Orbit Determination Parameters
   # obs. used (total)      14  
   data-arc span      1 day  
   first obs. used      2007-03-20  
   last obs. used      2007-03-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .41321  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:06:38  

Additional Information
 Earth MOID = .0145731 au 
 Jupiter MOID = 3.833 au 
 T_jup = 5.397 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 3.880114256436873E-5 3.169824255138904E-5 -.0080676043566333 .001068857324007812 -.01192918644108092 .002673015842610789
q 3.169824255138904E-5 4.446956961522595E-5 -.00857576820374064 .0009871042273650167 -.01385523879003383 .002211602560548052
tp -.0080676043566333 -.00857576820374064 1.889570957530285 -.2344121725450011 2.919555203566214 -.558759840721459
node .001068857324007812 .0009871042273650167 -.2344121725450011 .03014264694375565 -.3538183731034701 .07380532963686365
peri -.01192918644108092 -.01385523879003383 2.919555203566214 -.3538183731034701 4.576920019842007 -.8279772112314971
i .002673015842610789 .002211602560548052 -.558759840721459 .07380532963686365 -.8279772112314971 .1841892599920065

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 20.0   n/a MPO118244  

[ hide close-approach data ]
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
2007-Mar-30 03:55 02:31 Earth 0.157774382568644 0.147544566834384 0.168005457557688 19.5528721896559 19.552008465833 2454189.663352204 150.69453845913 510635.476551922 16163.5986511756 2.58037562305333 64.2422621309364 T 7 CATAB v2.0e-lin.ifort 2017-Nov-28 07:45:51 2018-Dec-11 15:02
2068-Oct-11 08:01 4_03:05 Earth 0.164064105191932 0.154371287184011 0.189282830549332 20.1164464774499 20.115639137894 2476665.833954810 5945.04955837408 2807691.07930044 143151.762726501 -72.0048557572834 175.294790834347 T 7 CATAB v2.0e-lin.ifort 2017-Nov-28 07:45:51 2018-Dec-11 15:02
2187-Mar-31 14:18 5_11:17 Earth 0.180756899596734 0.0780835431204802 0.324243244752373 20.0061799658943 20.0054431460744 2519935.096115006 7876.56281697238 7553169.30456344 28978.6790987087 25.2727362212926 281.358435699255 T 7 CATAB v2.0e-lin.ifort 2017-Nov-28 07:45:51 2018-Dec-11 15:02
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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