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3723 Voznesenskij (1976 GK2)
Classification: Main-belt Asteroid          SPK-ID: 2003723
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1109746329464186 2.5911e-08  
a 2.254957496869286 5.9707e-09 au
q 2.004714416344442 6.0095e-08 au
i 1.377955020734243 2.713e-06 deg
node 95.02491928635519 0.00015774 deg
peri 168.5249905325338 0.00015873 deg
M 317.6754789955212 1.8389e-05 deg
tp 2459145.910416529091
(2020-Oct-23.41041653)
6.3208e-05 TDB
period 1236.818485079446
3.39
4.9123e-06
1.345e-08
d
yr
n .2910693883887705 1.156e-09 deg/d
Q 2.505200577394129 6.6333e-09 au
  Orbit Determination Parameters
   # obs. used (total)      2427  
   data-arc span      23966 days (65.62 yr)  
   first obs. used      1954-12-22  
   last obs. used      2020-08-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49076  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-24 23:07:09  

Additional Information
 Earth MOID = .989024 au 
 Jupiter MOID = 2.54489 au 
 T_jup = 3.616 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456905.5 (2014-Sep-05.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1114197787626612 2.5871e-08  
q 2.003957600553403 6.0048e-08 au
tp 2456671.632513407536
(2014-Jan-14.13251341)
6.3142e-05 TDB
node 95.02844608169012 0.00015772 deg
peri 168.4865760465814 0.00015871 deg
i 1.378026784927825 2.7132e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      2427  
   data-arc span      23966 days (65.62 yr)  
   first obs. used      1954-12-22  
   last obs. used      2020-08-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49076  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-24 23:07:09  

Additional Information
 Jupiter MOID = 2.54489 au 
 T_jup = 3.616 
Orbit Covariance (6×6)
  e q tp node peri i
e 6.69313767784005E-16 -1.547877125524332E-15 -2.261522666562383E-13 -1.879000897404088E-16 -5.155912398925991E-14 -1.44692577290434E-16
q -1.547877125524332E-15 3.605799471164395E-15 4.773842585336613E-13 6.787043079078634E-16 1.069721520031739E-13 3.504697299242097E-16
tp -2.261522666562383E-13 4.773842585336613E-13 3.986911219018997E-9 1.846956379822312E-11 1.132293908975987E-9 5.62012656870208E-13
node -1.879000897404088E-16 6.787043079078634E-16 1.846956379822312E-11 2.487541351419445E-8 -2.486267917220418E-8 4.297510237762134E-12
peri -5.155912398925991E-14 1.069721520031739E-13 1.132293908975987E-9 -2.486267917220418E-8 2.518763605138144E-8 -4.13720796761117E-12
i -1.44692577290434E-16 3.504697299242097E-16 5.62012656870208E-13 4.297510237762134E-12 -4.13720796761117E-12 7.361414166625477E-12

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 14.0   n/a MPO309177  
diameter diameter 9.748 km 0.037 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
rotation period rot_per 7.964 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Waszczak, A.; Chang, C.-K.; Ofeck, E.O.; Laher, F.; et al. (2015) Astron. J. 150, A75.]
geometric albedo albedo 0.042   0.002 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

3723 Voznesenskij (1976 GK2)          Discovered 1976-Apr-01 by Chernykh, N. at Nauchnyj
Reference: DISCOVERY.DBLast Updated: 2003-08-29

[ show close-approach data ]
Alternate Designations
 1976 GK2 = 1986 EE1 = 1986 ES3 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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