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14079 (1997 FV3)
Classification: Main-belt Asteroid          SPK-ID: 2014079
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1297134015377671 3.2e-08  
a 2.311022944215561 7.0778e-09 au
q 2.011252297089535 7.3608e-08 au
i 7.326168871707785 4.0662e-06 deg
node .2557223394724504 3.0484e-05 deg
peri 17.04800020065251 3.4935e-05 deg
M 86.67024526090621 1.7293e-05 deg
tp 2458891.561283788204
(2020-Feb-12.06128379)
6.1376e-05 TDB
period 1283.230911617286
3.51
5.8951e-06
1.614e-08
d
yr
n .2805418703219077 1.2888e-09 deg/d
Q 2.610793591341587 7.9959e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1641  
   data-arc span      10813 days (29.60 yr)  
   first obs. used      1991-08-06  
   last obs. used      2021-03-14  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .51158  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 00:16:56  

Additional Information
 Earth MOID = 1.01202 au 
 Jupiter MOID = 2.8609 au 
 T_jup = 3.562 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457205.5 (2015-Jul-02.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1307480807527134 3.2154e-08  
q 2.008242938506975 7.4052e-08 au
tp 2457607.471427762941
(2016-Aug-06.97142776)
5.9688e-05 TDB
node .3437572331953167 3.0446e-05 deg
peri 16.71343334766871 3.4802e-05 deg
i 7.33274099954236 4.0681e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1641  
   data-arc span      10813 days (29.60 yr)  
   first obs. used      1991-08-06  
   last obs. used      2021-03-14  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .51158  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 00:16:56  

Additional Information
 Jupiter MOID = 2.8609 au 
 T_jup = 3.562 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.033854072063342E-15 -2.372881436810099E-15 -5.196403076535122E-13 4.804079516858416E-15 -1.589980433234304E-13 -8.576125861111625E-16
q -2.372881436810099E-15 5.483653415407227E-15 1.235690099336697E-12 -1.109769829364365E-14 3.731857474240025E-13 2.021915429996693E-15
tp -5.196403076535122E-13 1.235690099336697E-12 3.562638354044303E-9 1.208575060243855E-12 1.020394886322729E-9 -6.521259517873047E-13
node 4.804079516858416E-15 -1.109769829364365E-14 1.208575060243855E-12 9.269798852435498E-10 -9.184295002444025E-10 -3.650769354040487E-11
peri -1.589980433234304E-13 3.731857474240025E-13 1.020394886322729E-9 -9.184295002444025E-10 1.211160413636304E-9 3.602178871210063E-11
i -8.576125861111625E-16 2.021915429996693E-15 -6.521259517873047E-13 -3.650769354040487E-11 3.602178871210063E-11 1.654914246509817E-11

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 14.7   n/a MPO526085  
diameter diameter 2.296 km 0.361 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.582   0.110 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

14079 (1997 FV3)          Discovered 1997-Mar-31 by LINEAR at Socorro
Reference: 20000320/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 1997 FV3 = 2000 AV66 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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