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19612 Noordung (1999 OO)
Classification: Main-belt Asteroid          SPK-ID: 2019612
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .119973427988364 2.1933e-08  
a 2.385139501198229 8.1752e-09 au
q 2.098986139009021 5.2348e-08 au
i 5.887821564355174 7.7189e-07 deg
node 275.4918269804277 9.8587e-06 deg
peri 19.3978807123399 1.3202e-05 deg
M 293.7022423730573 8.9365e-06 deg
tp 2459448.279540481341
(2021-Aug-21.77954048)
3.418e-05 TDB
period 1345.454775034996
3.68
6.9175e-06
1.894e-08
d
yr
n .2675675219114193 1.3757e-09 deg/d
Q 2.671292863387437 9.156e-09 au
  Orbit Determination Parameters
   # obs. used (total)      2094  
   data-arc span      11626 days (31.83 yr)  
   first obs. used      1988-08-11  
   last obs. used      2020-06-10  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .47312  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 02:59:22  

Additional Information
 Earth MOID = 1.08195 au 
 Jupiter MOID = 2.49093 au 
 T_jup = 3.519 
[ show covariance matrix ]

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 14.02   n/a E2021B10  
diameter diameter 3.715 km 0.237 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.352   0.060 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

19612 Noordung           Discovered 1999 July 17 at the Črni Vrh Observatory.
At the end of 1928 Herman Potočnik (1892-1929) published under the pseudonym Hermann Noordung a visionary work entitled Das Problem der Befahrung des Weltraums---der Raketen-motor. In this work he was the first to detail a technical description of a space station in a geostationary orbit and its applications.
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character)
Reference: 20070402/MPCPages.arcLast Updated: 2007-07-05

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Alternate Designations
 1999 OO = 1994 BE3 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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