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(2020 FX3)
Classification: Apollo [NEO]          SPK-ID: 54016336
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 .5071608564544721 0.00041742  
a 1.851792723940968 0.001443 au
q .912635940090907 6.1812e-05 au
i 4.535643734978557 0.0032644 deg
node 3.148236290860205 0.0013585 deg
peri 242.6334068453751 0.0036456 deg
M 5.48061024572888 0.0049005 deg
tp 2458986.487571667797
(2020-May-16.98757167)
0.0038513 TDB
period 920.4219919714836
2.52
1.0758
0.002945
d
yr
n .3911249439280602 0.00045717 deg/d
Q 2.790949507791029 0.0021748 au
  Orbit Determination Parameters
   # obs. used (total)      66  
   data-arc span      19 days  
   first obs. used      2020-03-23  
   last obs. used      2020-04-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .47706  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-29 07:48:20  

Additional Information
 Earth MOID = .0259384 au 
 Jupiter MOID = 2.26945 au 
 T_jup = 3.835 
[ 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 24.09   .51728 8 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
2010-Mar-14 06:32 9_19:48 Earth 0.421099761773025 0.2283235970141 0.613972424913234 23.3253737757228 23.3251025060306 2455269.772101422 14147.7973644699 9620627.13411313 56.2506593279027 1.70742370670211 30065.7571903786 T 8 CATAB v2.0f-lin.ifort 2020-Aug-29 07:48:29 2020-Aug-29 07:48
2013-Jan-24 17:28 7_14:32 Mars 0.0106362613478429 0.00698889912285664 0.151660008984883 12.8972267724323 12.8951396112306 2456317.227507810 10952.3914289225 7154913.45651625 59.5547407187869 -41.0902056786084 17514.8337727019 T 8 CATAB v2.0f-lin.ifort 2020-Aug-29 07:48:29 2020-Aug-29 07:48
2015-Mar-27 07:57 6_22:44 Earth 0.185806524650168 0.0767389977358764 0.296130327163624 16.374923635769 16.3740478785487 2457108.831293712 10004.1504444374 5522969.54896692 49.255768592607 6.4166049493324 55482.8871755089 T 8 CATAB v2.0f-lin.ifort 2020-Aug-29 07:48:29 2020-Aug-29 07:48
2020-Apr-15 01:01 < 00:01 Earth 0.0361065922762781 0.03602625137839 0.0361869326808337 10.250843627329 10.2436421960022 2458954.542701656 0.159538373018917 4000.72770356587 12.1079861190643 -0.126759414052802 879.281573644083 T 8 CATAB v2.0f-lin.ifort 2020-Aug-29 07:48:29 2020-Aug-29 07:48
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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