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JPL Small-Body Database Browser
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19414 (1998 FP32)
Classification: Main-belt Asteroid          SPK-ID: 2019414
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2296527211605967 3.8358e-08  
a 2.345579881639399 9.1865e-09 au
q 1.80691107912136 8.8875e-08 au
i 2.827183542211815 3.6964e-06 deg
node 332.0575717592947 7.4681e-05 deg
peri 28.75349478577379 7.5251e-05 deg
M 236.0028216454335 1.2557e-05 deg
tp 2459452.442382402500
(2021-Aug-25.94238240)
4.7614e-05 TDB
period 1312.120645194569
3.59
7.7084e-06
2.11e-08
d
yr
n .2743650146184667 1.6118e-09 deg/d
Q 2.884248684157437 1.1296e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1688  
   data-arc span      25783 days (70.59 yr)  
   first obs. used      1949-09-25  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .46531  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 05:00:51  

Additional Information
 Earth MOID = .804365 au 
 Jupiter MOID = 2.5741 au 
 T_jup = 3.524 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 14.1   n/a MPO324488  
diameter diameter 5.230 km 0.090 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.194   0.041 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

19414 (1998 FP32)          Discovered 1998-Mar-20 by LINEAR at Socorro
Reference: 20001211/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1998 FP32 = 1949 SJ1 = 1967 TP = 1978 RT16 = 1978 VT2 = 1980 FD6 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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