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(2017 FZ2)
Classification: Apollo [NEO]          SPK-ID: 3771633
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2640944338750831 1.8534e-06  
a 1.00783166343353 6.0031e-08 au
q .7416689308376689 1.826e-06 au
i 1.812322804786765 1.1377e-05 deg
node 185.8060753083035 1.9289e-05 deg
peri 100.1587346930026 0.00010874 deg
M 342.0374998262971 3.394e-05 deg
tp 2459018.939311855073
(2020-Jun-18.43931186)
3.5971e-05 TDB
period 369.5561421646951
1.01
3.3019e-05
9.04e-08
d
yr
n .9741415685618983 8.7037e-08 deg/d
Q 1.273994396029392 7.5885e-08 au
  Orbit Determination Parameters
   # obs. used (total)      162  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      360 days  
   first obs. used      2017-03-19  
   last obs. used      2018-03-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .34178  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Mar-14 11:12:02  

Additional Information
 Earth MOID = .0015941 au 
 Jupiter MOID = 3.85554 au 
 T_jup = 6.011 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457849.5 (2017-Apr-06.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2640689137823792 1.8483e-06  
q .7411318242908288 1.8148e-06 au
tp 2457910.955075958219
(2017-Jun-06.45507596)
9.936e-05 TDB
node 185.8947201874442 1.9201e-05 deg
peri 100.2796965323591 0.00010244 deg
i 1.811720927820546 1.1355e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      162  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      360 days  
   first obs. used      2017-03-19  
   last obs. used      2018-03-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .34178  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Mar-14 11:12:02  

Additional Information
 Jupiter MOID = 3.85554 au 
 T_jup = 6.011 
Orbit Covariance (6×6)
  e q tp node peri i
e 3.416238216584811E-12 -3.35423810446284E-12 -1.835619193710281E-10 1.830222060478323E-11 1.868549481427832E-10 1.413846332547616E-11
q -3.35423810446284E-12 3.293623858513364E-12 1.801948006692552E-10 -1.798795610761375E-11 -1.835173259910986E-10 -1.387368085527416E-11
tp -1.835619193710281E-10 1.801948006692552E-10 9.872465375997993E-9 -9.718161529143104E-10 -1.003803549183854E-8 -7.61059762284259E-10
node 1.830222060478323E-11 -1.798795610761375E-11 -9.718161529143104E-10 3.686778301552889E-10 7.404881025644284E-10 -4.926264986231183E-11
peri 1.868549481427832E-10 -1.835173259910986E-10 -1.003803549183854E-8 7.404881025644284E-10 1.049398090469213E-8 8.965110816643286E-10
i 1.413846332547616E-11 -1.387368085527416E-11 -7.61059762284259E-10 -4.926264986231183E-11 8.965110816643286E-10 1.289457336965729E-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 26.6   n/a MPO438993  

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