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JPL Small-Body Database Browser
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(2015 FF36)
Classification: Apollo [NEO]          SPK-ID: 3714122
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5337041410159989 0.00018884  
a 2.087254141879355 0.00071119 au
q .9732779630055476 6.2535e-05 au
i .1772053069360129 5.1957e-05 deg
node 6.1016314008362 0.12787 deg
peri 205.4709182867212 0.13238 deg
M 120.8835633655799 0.4372 deg
tp 2458230.649528324064
(2018-Apr-22.14952832)
1.1486 TDB
period 1101.44147058829
3.02
0.56294
0.001541
d
yr
n .3268444212543773 0.00016705 deg/d
Q 3.201230320753162 0.0010908 au
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      12 days  
   first obs. used      2015-03-14  
   last obs. used      2015-03-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .40095  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:52  

Additional Information
 Earth MOID = .000183162 au 
 Jupiter MOID = 1.7679 au 
 T_jup = 3.564 
[ 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 26.6   n/a MPO332802  

[ 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
1951-Feb-16 05:40 1_05:20 Earth 0.443193735302957 0.388888898194724 0.497507805010646 22.638641513496 22.6383759484398 2433693.736149532 1759.4968707864 2710070.76498307 5.1760807474044 -2.13550374502283 444653.250114768 T 6 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:46 2018-Dec-11 16:36
2012-Feb-27 14:26 2_21:41 Earth 0.285636266215726 0.225745459583297 0.345535723117994 17.5139851427032 17.5134525188205 2455985.101556820 4181.02977426888 2987756.46790049 4.24355441605402 -1.52538831006132 244126.130251678 T 6 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:46 2018-Dec-11 16:36
2015-Mar-28 06:16 < 00:01 Earth 0.00907601162870476 0.00906142111052797 0.00909060179137 8.81072149582196 8.77733818715022 2457109.761432599 0.0651863426713863 722.005351748682 1.65186342078023 -0.192272228741628 1150.35541387146 T 6 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:46 2018-Dec-11 16:36
2018-Jul-16 23:53 2_19:48 Mars 0.0776117356892632 0.0411357194872031 0.124660216928595 15.5949267434293 15.594690206614 2458316.495267795 4068.20570814413 2539047.80666262 26.6164595104402 -28.8297557716279 208754.936122535 T 6 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:46 2018-Dec-11 16:36
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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