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(2020 FL6)
Classification: Apollo [NEO]          SPK-ID: 54016411
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4852903393712621 0.00055516  
a 1.658125236369596 0.0015535 au
q .8534530776917402 0.00012094 au
i 3.402006039114022 0.0034536 deg
node 3.024239548984865 0.00034383 deg
peri 249.1879091797776 0.001554 deg
M 6.68468494889595 0.0042276 deg
tp 2458986.018856285249
(2020-May-16.51885629)
0.011192 TDB
period 779.8739622233433
2.14
1.096
0.003001
d
yr
n .461613052157397 0.00064871 deg/d
Q 2.462797395047451 0.0023073 au
  Orbit Determination Parameters
   # obs. used (total)      80  
   data-arc span      8 days  
   first obs. used      2020-03-26  
   last obs. used      2020-04-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .30547  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-04 06:26:06  

Additional Information
 Earth MOID = .0127256 au 
 Jupiter MOID = 2.60556 au 
 T_jup = 4.124 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458937.5 (2020-Mar-29.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4856957824137468 0.00055452  
q .8537614313271229 0.00012159 au
tp 2458985.975478270706
(2020-May-16.47547827)
0.011045 TDB
node 3.231823984317207 0.00031226 deg
peri 248.9096003591796 0.0024027 deg
i 3.456284704061034 0.0033373 deg
  Orbit Determination Parameters
   # obs. used (total)      80  
   data-arc span      8 days  
   first obs. used      2020-03-26  
   last obs. used      2020-04-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .30547  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-04 06:26:06  

Additional Information
 Jupiter MOID = 2.60556 au 
 T_jup = 4.124 
Orbit Covariance (6×6)
  e q tp node peri i
e 3.074885205850854E-7 -6.74241704558959E-8 -6.124674807565958E-6 -1.700047238358888E-7 1.330192996069537E-6 1.850401991962602E-6
q -6.74241704558959E-8 1.478466627495366E-8 1.34295270043793E-6 3.729330471191821E-8 -2.917479399664312E-7 -4.057300414829068E-7
tp -6.124674807565958E-6 1.34295270043793E-6 .0001219963141257528 3.385143057359445E-6 -2.648905442767111E-5 -3.685794814963993E-5
node -1.700047238358888E-7 3.729330471191821E-8 3.385143057359445E-6 9.750349559792419E-8 -7.414123394462428E-7 -1.020702337255752E-6
peri 1.330192996069537E-6 -2.917479399664312E-7 -2.648905442767111E-5 -7.414123394462428E-7 5.77296732910245E-6 8.000258458942328E-6
i 1.850401991962602E-6 -4.057300414829068E-7 -3.685794814963993E-5 -1.020702337255752E-6 8.000258458942328E-6 1.113727367457797E-5

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 25.251   .36627 6 autocmod 2.8

[ 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
2015-Sep-26 15:33 4_03:55 Mars 0.0796144307248671 0.0227185157057456 0.16164723963665 13.441350303962 13.4410827719135 2457292.148050773 5995.339578672 4175721.20932093 152.831503758078 -16.5821810548454 21998.4997638596 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2020-Apr-04 14:21 < 00:01 Earth 0.0129447548359812 0.0129056368625414 0.0129838721434736 12.0667291263018 12.0496590187394 2458944.097570805 0.0560727845517119 1945.12839693902 4.99340556616612 -0.106679347403875 678.822510093427 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2022-Aug-21 02:43 3_00:27 Earth 0.239331140664214 0.186060071781123 0.293056231969266 18.8235098060256 18.8229183542166 2459812.613510713 4347.42520532963 2717928.39089613 92.1460795136622 10.7535804558997 66676.4308694257 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2088-Sep-18 00:52 1_08:39 Venus 0.136031201195673 0.124697911052652 0.151312410148097 4.66369534976383 4.6602711451823 2483947.536304316 1958.5178841976 1336576.93226501 85.1044869719956 -59.7328497351165 840421.692765322 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2094-Sep-30 23:20 00:47 Mars 0.0377052798148454 0.0347285508121743 0.0407124830837218 11.8451334139486 11.8444923876995 2486151.472224421 47.2785707549661 158485.892213412 192.28925653496 19.64780349154 9919.26391033844 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2099-Aug-27 06:00 2_08:23 Mars 0.0337270781672501 0.0246857673959107 0.0914947003802386 11.8618912236333 11.8611755967761 2487942.750022244 3383.48691867003 3247376.6877524 53.7374857431473 47.0517388947117 68785.642398037 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2101-Aug-28 15:17 4_19:22 Earth 0.349987004103821 0.25142176095937 0.448997159003524 22.1514832864724 22.1511396011421 2488674.137085650 6921.82226326163 4965300.92189925 84.560064920556 6.91298827061324 68573.3518974587 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2129-Apr-28 02:49 2_21:12 Venus 0.147323845698781 0.110199658774131 0.285993423462155 5.30298210385705 5.30020181704562 2498778.617068662 4152.17174758497 8284952.95584201 112.794961800911 48.4774137155184 156324.511764023 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2141-Oct-10 22:25 5_06:28 Mars 0.056342777403152 0.0180229433324653 0.16412481471902 11.5326432441197 11.5322026411969 2503327.433755785 7587.77885449423 5472836.72497824 154.075641751746 18.6598372414595 17684.1690342825 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2146-Sep-06 11:39 4_05:09 Mars 0.0266789182233752 0.0256200111233255 0.109941583765044 12.3934825472867 12.3926166631508 2505118.985092790 6068.62784358174 4960561.45257411 56.8196102976603 -73.812806216858 67151.2932653911 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2161-Apr-09 11:37 3_04:44 Earth 0.0244630061699873 0.0148070347859015 0.0483917706793834 11.4550489534732 11.4455366446915 2510447.984288618 4603.76219048515 1326596.90527298 9.41847434506031 -37.2670559860041 213662.549421407 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2163-Aug-27 04:58 11:26 Earth 0.303934359309104 0.291245822563691 0.316630852165888 20.7786977443427 20.7782758354871 2511317.707189818 686.392993533457 637656.977706774 90.5394154489897 6.98615272485461 56015.6831695112 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
2176-Apr-06 07:07 9_14:51 Earth 0.0194580933013263 0.0159140518212555 0.112725297993554 12.3252311396398 12.314116052452 2515923.796668769 13851.302255027 5007055.45041045 21.7504001770711 54.8948124079295 111983.594628612 T 6 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:14 2020-Apr-04 06:26
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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