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JPL Small-Body Database Browser
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(2015 FL35)
Classification: Apollo [NEO]          SPK-ID: 3713996
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2206003536712876 0.00041852  
a 1.2842743663394 0.00072227 au
q 1.000962986913959 3.5651e-05 au
i 24.39258824892467 0.021882 deg
node 3.82750545771605 0.00035378 deg
peri 208.5449580390862 0.025919 deg
M 273.8428028255787 0.82379 deg
tp 2458727.725512723851
(2019-Sep-01.22551272)
1.3238 TDB
period 531.6002154511121
1.46
0.44846
0.001228
d
yr
n .6772006284732345 0.00057128 deg/d
Q 1.56758574576484 0.00088161 au
  Orbit Determination Parameters
   # obs. used (total)      53  
   data-arc span      1 day  
   first obs. used      2015-03-22  
   last obs. used      2015-03-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .651  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:55  

Additional Information
 Earth MOID = .025776 au 
 Jupiter MOID = 3.41969 au 
 T_jup = 4.934 
[ 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 MPO332800  

[ 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
1996-Apr-16 05:05 7_05:17 Earth 0.429489492615753 0.171657725453616 0.713016447892746 16.1732495828594 16.1728659925077 2450189.711976100 10397.284842915 14492747.8172684 5433.09612083919 -16.4267201018264 3028.89780244271 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2015-Mar-25 13:35 < 00:01 Earth 0.0261556585477503 0.0260736564615075 0.0262376605881691 13.750295342854 13.742884771113 2457107.065726148 0.545331302457993 4088.80048865879 470.370344137703 -2.49528119023167 728.228379486411 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2015-Aug-13 16:00 08:01 Earth 0.450447474938046 0.448021780641506 0.452874648338124 11.5747608050392 11.5742497522503 2457248.166493190 481.01224166089 127829.657895183 19335.5442551944 19.0586470883671 893.643269533963 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2018-Sep-12 18:42 5_03:54 Earth 0.477528056342332 0.475462575927572 0.483909070944147 13.0695291306586 13.0691021967826 2458374.279196676 7433.56456870525 2282431.86603395 3325.44037806944 -84.6970012399181 35197.5474070612 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2034-Mar-04 01:38 6_07:33 Earth 0.490808021771398 0.23724563310376 0.744441517224026 22.0855943312206 22.0853485243428 2464025.567981478 9093.19988393126 12649334.9566304 291.287149942836 1.17379640162323 4741.50187404438 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2050-Mar-10 01:03 8_10:45 Earth 0.355328160433313 0.0848088305066049 0.632524001941191 19.0733608243729 19.0729676728335 2469875.543425817 12164.941185848 13871470.5317 594.490157017603 6.42810944014316 10788.6598033396 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2063-Apr-11 22:07 8_00:53 Earth 0.341368009698997 0.16628604813817 0.613150200616979 14.8197264383142 14.8191997458954 2474656.421722376 11573.4892571601 14561413.47572 6283.79004021069 -29.1315154704338 3657.19390176164 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2066-Mar-16 14:56 9_11:37 Earth 0.205990532706408 0.0501680156282439 0.4580216245184 16.2339351857822 16.2331383809731 2475726.122150907 13657.0736831298 12739717.2812948 1115.6424419897 14.1031705730517 7487.20539565194 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2079-Apr-20 14:41 4_01:27 Earth 0.480669221569557 0.301584773139346 0.661491208592173 17.0269186380137 17.0265930756943 2480509.111561816 5847.3974355828 9088624.03884593 4724.61020117092 -8.46600673987286 1987.73895846201 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2082-Mar-22 18:33 7_11:49 Earth 0.0710214172911679 0.0328410222124912 0.243680354614292 14.3130892226056 14.3104678460268 2481576.273161234 10789.1551312504 8900871.76623439 1105.45315924757 27.5689570390291 4937.98821587304 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2098-Mar-26 03:15 2_14:10 Earth 0.0270184565374518 0.0260830415684394 0.0726822306065324 13.6648552997138 13.657636557861 2487423.635422613 3730.21702417481 3032543.65307462 198.166006882484 -74.9146485221784 34964.6399057667 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
2098-Aug-13 07:04 6_11:40 Earth 0.448752654804752 0.442543769964273 0.461775296525581 11.5737242986694 11.5732112697833 2487563.794722361 9340.08048551099 2804329.38239402 5164.58044151344 80.0831790391448 14621.962387531 T 4 CATAB v2.0e-lin.ifort 2017-Nov-30 04:26:23 2018-Dec-11 16:36
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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