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(2020 FQ6)
Classification: Apollo [NEO]          SPK-ID: 54016413
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458935.5 (2020-Mar-27.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .536875811697294 0.0021473  
a 2.07570196965513 0.0094112 au
q .9613077898548599 9.871e-05 au
i 6.442381263105323 0.018426 deg
node 190.4026822733148 0.0035925 deg
peri 43.31686338409428 0.005968 deg
M 347.2922538026204 0.092389 deg
tp 2458974.057774104600
(2020-May-04.55777410)
0.018096 TDB
period 1092.310033742907
2.99
7.4287
0.02034
d
yr
n .3295767583187209 0.0022414 deg/d
Q 3.190096149455399 0.014464 au
  Orbit Determination Parameters
   # obs. used (total)      36  
   data-arc span      15 days  
   first obs. used      2020-03-22  
   last obs. used      2020-04-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .41701  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-08 06:20:15  

Additional Information
 Earth MOID = .0256494 au 
 Jupiter MOID = 1.83032 au 
 T_jup = 3.566 
[ 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 24.925   .56705 9 autocmod 2.8

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2020-Apr-06 04:39 < 00:01 Earth 0.0458726455660925 0.0454179598652947 0.0463273229765324 11.2366816692792 11.2315113136075 2458945.694070545 0.0821660239600423 22652.2574309184 9.66775112170173 -0.0492687220655316 202.218424563055 T 9 CATAB v2.0f-lin.ifort 2020-Apr-08 06:20:16 2020-Apr-08 06:20
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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