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(2020 FP)
Classification: Apollo [NEO]          SPK-ID: 54016207
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458930.5 (2020-Mar-22.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5480445287609799 0.0015948  
a 2.180408083678061 0.0076334 au
q .9854473629520871 2.7504e-05 au
i 2.947910660037418 0.0066053 deg
node 169.4990359050561 0.00055848 deg
peri 44.42222393900642 0.010489 deg
M 351.9511872731704 0.04387 deg
tp 2458956.792653859593
(2020-Apr-17.29265386)
0.0052707 TDB
period 1175.993989511275
3.22
6.1755
0.01691
d
yr
n .3061240135671189 0.0016076 deg/d
Q 3.375368804404035 0.011817 au
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      8 days  
   first obs. used      2020-03-16  
   last obs. used      2020-03-24  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .3186  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-04 06:25:58  

Additional Information
 Earth MOID = .0224013 au 
 Jupiter MOID = 1.59479 au 
 T_jup = 3.468 
[ 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 25.879   .40365 4 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-Mar-27 00:39 < 00:01 Earth 0.0376781507359486 0.0373945925244333 0.0379617022080422 9.45486127955433 9.44737890411305 2458935.527246592 0.206763268742981 14117.3701621881 7.67919771059793 8.16775506526229e-05 252.034175042382 T 4 CATAB v2.0f-lin.ifort 2020-Apr-04 06:26:00 2020-Apr-04 06:26
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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