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78150 (2002 NO24)
Classification: Main-belt Asteroid          SPK-ID: 2078150
[ 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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1715652693120984 3.6618e-08  
a 3.170421177237255 1.7502e-08 au
q 2.626487014131765 1.1271e-07 au
i 28.72130837591587 4.3054e-06 deg
node 142.9497303848179 8.0167e-06 deg
peri 204.7593052452134 1.5191e-05 deg
M 72.65588263611843 1.204e-05 deg
tp 2458784.357425616820
(2019-Oct-27.85742562)		 6.8776e-05 TDB
period 2061.929761809417
5.65		 1.7074e-05
4.675e-08		 d
yr
n .1745937260656673 1.4458e-09 deg/d
Q 3.714355340342745 2.0505e-08 au
   Orbit Determination Parameters
   # obs. used (total)      1430  
   data-arc span      7656 days (20.96 yr)  
   first obs. used      2000-02-03  
   last obs. used      2021-01-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52796  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 07:13:50  

Additional Information
 Earth MOID = 1.63239 au 
 Jupiter MOID = 1.71304 au 
 T_jup = 2.990 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457547.5 (2016-Jun-08.0) TDB
Reference: JPL 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .173567260857689 3.7025e-08  
q 2.617729498538037 1.1459e-07 au
tp 2456720.457549093023
(2014-Mar-03.95754909)		 6.7937e-05 TDB
node 143.1627816044729 8.0181e-06 deg
peri 204.0667298357773 1.4939e-05 deg
i 28.77594951552407 4.3017e-06 deg
   Orbit Determination Parameters
   # obs. used (total)      1430  
   data-arc span      7656 days (20.96 yr)  
   first obs. used      2000-02-03  
   last obs. used      2021-01-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52796  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 07:13:50  

Additional Information
 Jupiter MOID = 1.71304 au 
 T_jup = 2.990 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.37086620074248E-15 -4.21179279008586E-15 -6.755804652727672E-13 3.225938144194814E-15 -1.592221778209108E-13 4.801977408618679E-16
q -4.21179279008586E-15 1.313028718187291E-14 1.97626908847886E-12 -1.07249489832141E-14 4.898249850457318E-13 3.98589325340341E-17
tp -6.755804652727672E-13 1.97626908847886E-12 4.61539293167877E-9 -1.433526632046769E-11 8.708798668650857E-10 -6.780597489534835E-12
node 3.225938144194814E-15 -1.07249489832141E-14 -1.433526632046769E-11 6.429058299678162E-11 -5.840686840981364E-11 -7.078105613553777E-12
peri -1.592221778209108E-13 4.898249850457318E-13 8.708798668650857E-10 -5.840686840981364E-11 2.231691806281763E-10 4.747974965202599E-12
i 4.801977408618679E-16 3.98589325340341E-17 -6.780597489534835E-12 -7.078105613553777E-12 4.747974965202599E-12 1.85043206528391E-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 13.7   n/a MPO502627  
diameter diameter 10.169 km 0.199 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.075   0.011 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

78150 (2002 NO24)          Discovered 2002-Jul-09 by LINEAR at Socorro
Reference: 20040415/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 2002 NO24 = 2001 KW63 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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