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(2005 RC34)
Classification: Apollo [NEO, PHA]          SPK-ID: 3279825
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 56 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5132332478753686 2.3602e-08  
a 2.061153170554603 8.6885e-09 au
q 1.00330083446225 4.9878e-08 au
i 10.76914560360934 1.0342e-05 deg
node 290.9659992677483 8.3995e-06 deg
peri 36.11770632176295 1.7462e-05 deg
M 354.7538724516737 8.5844e-06 deg
tp 2459016.250711309274
(2020-Jun-15.75071131)
2.5862e-05 TDB
period 1080.846018154416
2.96
6.8342e-06
1.871e-08
d
yr
n .3330724210047175 2.106e-09 deg/d
Q 3.119005506646956 1.3148e-08 au
  Orbit Determination Parameters
   # obs. used (total)      368  
   # delay obs. used      2  
   # Doppler obs. used      2  
   data-arc span      2169 days (5.94 yr)  
   first obs. used      2005-06-09  
   last obs. used      2011-05-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .38643  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:10:31  

Additional Information
 Earth MOID = .0397912 au 
 Jupiter MOID = 2.29505 au 
 T_jup = 3.586 
[ hide covariance matrix ]
Orbital Elements at Epoch 2454298.5 (2007-Jul-17.0) TDB
Reference: JPL 56 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5141672163663544 2.3697e-08  
q 1.001354258112762 4.9944e-08 au
tp 2454692.858162920548
(2008-Aug-14.35816292)
1.2237e-05 TDB
node 291.217847070097 8.2872e-06 deg
peri 35.75636133793446 1.7205e-05 deg
i 10.81396263077106 1.0347e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      368  
   # delay obs. used      2  
   # Doppler obs. used      2  
   data-arc span      2169 days (5.94 yr)  
   first obs. used      2005-06-09  
   last obs. used      2011-05-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .38643  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:10:31  

Additional Information
 Jupiter MOID = 2.29505 au 
 T_jup = 3.586 
Orbit Covariance (6×6)
  e q tp node peri i
e 5.615573971912929E-16 -1.179247947148247E-15 2.805256140041264E-13 -2.456839588939348E-14 3.839896370719249E-13 -8.08173465877775E-14
q -1.179247947148247E-15 2.49444471680725E-15 -5.946824995898759E-13 4.428495276753141E-14 -8.070022404039361E-13 1.56122827038103E-13
tp 2.805256140041264E-13 -5.946824995898759E-13 1.497345533907292E-10 8.90459016968069E-12 1.825469321228434E-10 -2.857823361929011E-11
node -2.456839588939348E-14 4.428495276753141E-14 8.90459016968069E-12 6.867761419630499E-11 -5.940028371340749E-11 6.28233038932117E-11
peri 3.839896370719249E-13 -8.070022404039361E-13 1.825469321228434E-10 -5.940028371340749E-11 2.960133584404197E-10 -9.78157181788308E-11
i -8.08173465877775E-14 1.56122827038103E-13 -2.857823361929011E-11 6.28233038932117E-11 -9.78157181788308E-11 1.070568928582848E-10

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 19.7   n/a MPO264942  

[ show close-approach data ]
Alternate Designations
 2005 RC34 = 2005 LO40 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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