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34466 (2000 SN105)
Classification: Main-belt Asteroid          SPK-ID: 2034466
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09717055937436783 3.4037e-08  
a 3.017934282772563 2.2142e-08 au
q 2.724679920360472 1.0605e-07 au
i 2.26152019916358 4.0037e-06 deg
node 265.6829833045854 0.00011903 deg
peri 340.5985062563748 0.00012189 deg
M 95.56247275322485 2.5012e-05 deg
tp 2458888.167387832894
(2020-Feb-08.66738783)
0.00013348 TDB
period 1914.974938464877
5.24
2.1075e-05
5.77e-08
d
yr
n .1879920163804289 2.0689e-09 deg/d
Q 3.311188645184655 2.4294e-08 au
  Orbit Determination Parameters
   # obs. used (total)      952  
   data-arc span      9906 days (27.12 yr)  
   first obs. used      1993-04-16  
   last obs. used      2020-05-30  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .57318  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Aug-25 16:17:57  

Additional Information
 Earth MOID = 1.71147 au 
 Jupiter MOID = 1.70937 au 
 T_jup = 3.239 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456613.5 (2013-Nov-17.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09373663512720462 3.4388e-08  
q 2.734512385086757 1.0633e-07 au
tp 2456975.020124136397
(2014-Nov-13.52012414)
0.00014154 TDB
node 265.8373846849486 0.00011865 deg
peri 341.1146163459828 0.00012169 deg
i 2.264979885154098 4.0087e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      952  
   data-arc span      9906 days (27.12 yr)  
   first obs. used      1993-04-16  
   last obs. used      2020-05-30  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .57318  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Aug-25 16:17:57  

Additional Information
 Jupiter MOID = 1.70937 au 
 T_jup = 3.239 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.182510814995956E-15 -3.595722094899287E-15 -5.422814386562972E-15 5.937935763621901E-16 -1.91062371205684E-14 -2.853051683752856E-16
q -3.595722094899287E-15 1.130701981225683E-14 -6.844612586922137E-13 8.025540670234304E-15 -1.03671013157965E-13 1.140151653627425E-15
tp -5.422814386562972E-15 -6.844612586922137E-13 2.003247228447832E-8 3.282473548119392E-11 3.859473740158392E-9 -6.21026195936189E-13
node 5.937935763621901E-16 8.025540670234304E-15 3.282473548119392E-11 1.407897550357854E-8 -1.406093036344817E-8 5.492713629387326E-11
peri -1.91062371205684E-14 -1.03671013157965E-13 3.859473740158392E-9 -1.406093036344817E-8 1.480957564667986E-8 -5.500760324887698E-11
i -2.853051683752856E-16 1.140151653627425E-15 -6.21026195936189E-13 5.492713629387326E-11 -5.500760324887698E-11 1.60693174677972E-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 14.48   n/a MPO636567  
diameter diameter 5.684 km 0.106 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.104   0.011 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

34466 (2000 SN105)          Discovered 2000-Sep-24 by LINEAR at Socorro
Reference: 20020128/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 2000 SN105 = 1998 FY39 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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