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(2016 FM13)
Classification: Apollo [NEO]          SPK-ID: 3748482
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .534440769957664 0.00014253  
a 2.05258848964937 0.00059024 au
q .955601516834922 1.7904e-05 au
i 8.546603556563277 0.0022696 deg
node 199.7664078083903 0.0018799 deg
peri 61.67499917114972 0.0029956 deg
M 193.1182096517761 0.24459 deg
tp 2459698.417866603396
(2022-Apr-28.91786660)
0.94454 TDB
period 1074.116184894647
2.94
0.46331
0.001268
d
yr
n .3351592733288065 0.00014457 deg/d
Q 3.149575462463818 0.00090569 au
  Orbit Determination Parameters
   # obs. used (total)      23  
   data-arc span      37 days  
   first obs. used      2016-03-28  
   last obs. used      2016-05-04  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .19882  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 16:46:53  

Additional Information
 Earth MOID = .0643387 au 
 Jupiter MOID = 1.99844 au 
 T_jup = 3.585 
[ 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 24.0   n/a MPO380423  

[ 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
2013-Aug-09 13:52 1_17:29 Earth 0.231940672251904 0.214187738939769 0.250760072268165 15.4435190921982 15.4427752177597 2456514.077997545 2489.30378255259 1203038.35078784 510.497795645684 -40.5657108032766 36574.5058482926 T 7 CATAB v2.0g-lin.ifort 2021-Apr-15 16:46:54 2021-Apr-15 16:46
2016-May-26 00:01 00:04 Earth 0.123214521434004 0.1231083199889 0.123320722830059 8.85818841669944 8.85574686792689 2457534.500494287 3.526983453428 5294.41686452289 155.149351462114 1.13788921625986 2780.23500329505 T 7 CATAB v2.0g-lin.ifort 2021-Apr-15 16:46:54 2021-Apr-15 16:46
2019-Apr-14 18:51 1_10:34 Earth 0.243661621151001 0.219492852306078 0.267921755518961 17.749613938882 17.7489978493165 2458588.285237580 2074.09132187148 1230189.00131219 487.014817269235 -10.9797582789587 12543.1071285335 T 7 CATAB v2.0g-lin.ifort 2021-Apr-15 16:46:54 2021-Apr-15 16:46
2110-Aug-07 10:58 7_01:02 Earth 0.211507845260672 0.163659130501719 0.27684361086421 14.2352458878088 14.2343609058798 2491939.956849618 10141.6898411534 4165513.03222818 555.808095641572 -45.1363315221721 34188.0628969538 T 7 CATAB v2.0g-lin.ifort 2021-Apr-15 16:46:54 2021-Apr-15 16:46
2116-Apr-17 20:38 2_12:19 Earth 0.224887892603591 0.180391731176826 0.269869866279231 16.8587293259991 16.8580265280321 2494020.359742201 3619.48627530102 2291068.44137526 642.859187169221 -12.8943031038833 10402.4401585326 T 7 CATAB v2.0g-lin.ifort 2021-Apr-15 16:46:54 2021-Apr-15 16:46
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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