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(2017 MF)
Classification: Apollo [NEO]          SPK-ID: 3775253
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3686211110087957 2.897e-05  
a 1.573221976008442 6.898e-05 au
q .9932991433487568 2.0261e-06 au
i 1.37278130504508 0.00013976 deg
node 263.2115528175009 0.00016354 deg
peri 29.4534565637111 8.8276e-05 deg
M 166.7401962043776 0.036766 deg
tp 2458666.673168161552
(2019-Jul-02.17316816)
0.051653 TDB
period 720.7479791767585
1.97
0.047403
0.0001298
d
yr
n .4994811090711535 3.285e-05 deg/d
Q 2.153144808668126 9.4407e-05 au
  Orbit Determination Parameters
   # obs. used (total)      141  
   data-arc span      3 days  
   first obs. used      2017-06-18  
   last obs. used      2017-06-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .32384  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Jul-12 06:17:47  

Additional Information
 Earth MOID = .00241311 au 
 Jupiter MOID = 3.05231 au 
 T_jup = 4.329 
[ 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 MPO419561  

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