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(2016 CF194)
Classification: Amor [NEO]          SPK-ID: 3743610
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 40 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2040888663311324 2.2089e-06  
a 1.289823996378648 3.8822e-06 au
q 1.026585279191039 2.4114e-07 au
i 1.642764302278035 1.6708e-05 deg
node 114.961066211309 7.7408e-05 deg
peri 101.3195990025895 9.5091e-05 deg
M 58.24439966355077 0.0052358 deg
tp 2459113.934313390329
(2020-Sep-21.43431339)
0.0073908 TDB
period 535.049676183439
1.46
0.0024156
6.614e-06
d
yr
n .6728347217550241 3.0377e-06 deg/d
Q 1.553062713566257 4.6745e-06 au
  Orbit Determination Parameters
   # obs. used (total)      163  
   # delay obs. used      0  
   # Doppler obs. used      2  
   data-arc span      152 days  
   first obs. used      2016-01-31  
   last obs. used      2016-07-01  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      4  
   norm. resid. RMS      .48986  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 16:19:18  

Additional Information
 Earth MOID = .0331272 au 
 Jupiter MOID = 3.41204 au 
 T_jup = 5.009 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457489.5 (2016-Apr-11.0) TDB
Reference: JPL 40 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2032430981856042 2.2951e-06  
q 1.02622840725409 2.0952e-07 au
tp 2457508.212199754707
(2016-Apr-29.71219975)
6.3958e-05 TDB
node 115.5865994264724 5.1069e-05 deg
peri 100.3929928008261 7.1344e-05 deg
i 1.631622419616238 1.5519e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      163  
   # delay obs. used      0  
   # Doppler obs. used      2  
   data-arc span      152 days  
   first obs. used      2016-01-31  
   last obs. used      2016-07-01  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      4  
   norm. resid. RMS      .48986  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 16:19:18  

Additional Information
 Jupiter MOID = 3.41204 au 
 T_jup = 5.009 
Orbit Covariance (6×6)
  e q tp node peri i
e 5.26746997533564E-12 4.797781724838504E-13 1.453682655808615E-10 -4.57600907213628E-11 1.168047678874881E-10 3.554967265287894E-11
q 4.797781724838504E-13 4.390068373773452E-14 1.320349521868852E-11 -3.998143098130041E-12 1.042526237231773E-11 3.242260610335713E-12
tp 1.453682655808615E-10 1.320349521868852E-11 4.090678484825469E-9 -1.361861690214591E-9 3.401217118675325E-9 9.814073159956187E-10
node -4.57600907213628E-11 -3.998143098130041E-12 -1.361861690214591E-9 2.60800849361621E-9 -3.330038386413842E-9 -3.223574631461841E-10
peri 1.168047678874881E-10 1.042526237231773E-11 3.401217118675325E-9 -3.330038386413842E-9 5.089946873223803E-9 8.016790537917359E-10
i 3.554967265287894E-11 3.242260610335713E-12 9.814073159956187E-10 -3.223574631461841E-10 8.016790537917359E-10 2.408293374558747E-10

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 24.1   n/a MPO386963  

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