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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 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457480.5 (2016-Apr-02.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5343190542253041 0.00014616  
q .9559256928018682 1.5081e-05 au
tp 2457549.902191268760
(2016-Jun-10.40219127)
0.00083466 TDB
node 199.8250557069462 0.0017953 deg
peri 61.58701112640653 0.0025937 deg
i 8.551924153501901 0.0022765 deg
  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
 Jupiter MOID = 1.99844 au 
 T_jup = 3.585 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.136368902239532E-8 -2.182647384708885E-9 4.496017779049853E-8 -2.575194920005237E-7 3.504391354109941E-7 3.302189952756259E-7
q -2.182647384708885E-9 2.274246284918591E-10 -6.076940961012107E-9 2.690611619579084E-8 -3.771802919483553E-8 -3.42310005830375E-8
tp 4.496017779049853E-8 -6.076940961012107E-9 6.966637916859024E-7 -7.990069650945589E-7 1.501723791756393E-6 9.070276011682969E-7
node -2.575194920005237E-7 2.690611619579084E-8 -7.990069650945589E-7 3.223210998817801E-6 -4.556346229822074E-6 -4.075647438798066E-6
peri 3.504391354109941E-7 -3.771802919483553E-8 1.501723791756393E-6 -4.556346229822074E-6 6.72707884407632E-6 5.687907240610271E-6
i 3.302189952756259E-7 -3.42310005830375E-8 9.070276011682969E-7 -4.075647438798066E-6 5.687907240610271E-6 5.182632983559585E-6

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  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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