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36000 (1999 NV22)
Classification: Main-belt Asteroid          SPK-ID: 2036000
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 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1072956282750516 3.176e-08  
a 2.278475343864831 8.0848e-09 au
q 2.03400490033564 7.4154e-08 au
i 5.430500385176054 3.9479e-06 deg
node 121.4336884059424 4.0417e-05 deg
peri 114.9468884248419 4.5141e-05 deg
M 73.36314611090791 2.0649e-05 deg
tp 2458744.499759428615
(2019-Sep-17.99975943)
7.1782e-05 TDB
period 1256.217753616704
3.44
6.6863e-06
1.831e-08
d
yr
n .2865745201924944 1.5253e-09 deg/d
Q 2.522945787394022 8.9523e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1356  
   data-arc span      7881 days (21.58 yr)  
   first obs. used      1997-12-26  
   last obs. used      2019-07-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51082  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 04:01:08  

Additional Information
 Earth MOID = 1.02902 au 
 Jupiter MOID = 2.482 au 
 T_jup = 3.594 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456553.5 (2013-Sep-18.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1074940809352308 3.1775e-08  
q 2.033274642862609 7.4104e-08 au
tp 2456232.482831238030
(2012-Oct-31.98283124)
7.0276e-05 TDB
node 121.4628213392452 4.0423e-05 deg
peri 115.0465927204038 4.5121e-05 deg
i 5.430016086364611 3.9473e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1356  
   data-arc span      7881 days (21.58 yr)  
   first obs. used      1997-12-26  
   last obs. used      2019-07-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51082  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 04:01:08  

Additional Information
 Jupiter MOID = 2.482 au 
 T_jup = 3.594 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.009672237489194E-15 -2.344218072362949E-15 -2.985930775856922E-13 8.648984667166157E-17 -8.193343013882924E-14 -1.997573100303773E-16
q -2.344218072362949E-15 5.491447251916973E-15 6.797477405376864E-13 -2.919901814599198E-16 1.876025574897212E-13 6.586643070171875E-16
tp -2.985930775856922E-13 6.797477405376864E-13 4.938760463530826E-9 -2.641190586369947E-12 1.42196156575599E-9 4.691660487953595E-13
node 8.648984667166157E-17 -2.919901814599198E-16 -2.641190586369947E-12 1.634026381868026E-9 -1.627100858374443E-9 3.151683372993471E-11
peri -8.193343013882924E-14 1.876025574897212E-13 1.42196156575599E-9 -1.627100858374443E-9 2.035876298751082E-9 -3.123980078570683E-11
i -1.997573100303773E-16 6.586643070171875E-16 4.691660487953595E-13 3.151683372993471E-11 -3.123980078570683E-11 1.558147199526152E-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 15.1   n/a MPO474214  
diameter diameter 2.439 km 0.424 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.357   0.163 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

36000 (1999 NV22)          Discovered 1999-Jul-14 by LINEAR at Socorro
Reference: 20020227/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 1999 NV22 = 1998 BB38 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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