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34230 (2000 QF93)
Classification: Main-belt Asteroid          SPK-ID: 2034230
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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1507975808677075 3.4189e-08  
a 3.117530705511577 1.7872e-08 au
q 2.647414616839633 1.0343e-07 au
i 18.43249352514539 3.6797e-06 deg
node 168.3987448387734 1.2631e-05 deg
peri 289.4895684112876 1.8093e-05 deg
M 138.2385703913325 1.3863e-05 deg
tp 2458228.457391404004
(2018-Apr-19.95739140)
7.5417e-05 TDB
period 2010.548418634291
5.50
1.7289e-05
4.733e-08
d
yr
n .179055623164021 1.5397e-09 deg/d
Q 3.58764679418352 2.0567e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1854  
   data-arc span      8101 days (22.18 yr)  
   first obs. used      1998-05-26  
   last obs. used      2020-07-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .47452  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 03:01:32  

Additional Information
 Earth MOID = 1.72852 au 
 Jupiter MOID = 1.72299 au 
 T_jup = 3.121 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457441.5 (2016-Feb-23.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1521198779982766 3.4194e-08  
q 2.643345230149757 1.0367e-07 au
tp 2458228.687640049285
(2018-Apr-20.18764005)
7.4749e-05 TDB
node 168.424795459799 1.2629e-05 deg
peri 289.4709652197628 1.8e-05 deg
i 18.43549198381369 3.6803e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1854  
   data-arc span      8101 days (22.18 yr)  
   first obs. used      1998-05-26  
   last obs. used      2020-07-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .47452  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 03:01:32  

Additional Information
 Jupiter MOID = 1.72299 au 
 T_jup = 3.121 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.169195821090724E-15 -3.509019059261816E-15 -2.360702287749196E-13 -1.053620039634997E-16 -8.104702167251856E-14 1.509819443484289E-15
q -3.509019059261816E-15 1.074782668458134E-14 1.027395278372433E-12 9.838382141583124E-16 2.804883649612356E-13 -4.012466070397801E-15
tp -2.360702287749196E-13 1.027395278372433E-12 5.58742724494099E-9 2.211977386502452E-13 9.770273213176259E-10 -1.686597076134895E-12
node -1.053620039634997E-16 9.838382141583124E-16 2.211977386502452E-13 1.595000355716078E-10 -1.51016981180106E-10 1.023299026503591E-11
peri -8.104702167251856E-14 2.804883649612356E-13 9.770273213176259E-10 -1.51016981180106E-10 3.239848965100414E-10 -1.011006985205673E-11
i 1.509819443484289E-15 -4.012466070397801E-15 -1.686597076134895E-12 1.023299026503591E-11 -1.011006985205673E-11 1.354449635440422E-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 12.9   n/a MPO474195  
diameter diameter 13.484 km 0.354 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.089   0.017 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

34230 (2000 QF93)          Discovered 2000-Aug-25 by LINEAR at Socorro
Reference: 20020128/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 2000 QF93 = 1998 KB66 = 1999 NA60 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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