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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 
[ 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 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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