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3479 Malaparte (1980 TQ)
Classification: Main-belt Asteroid          SPK-ID: 2003479
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 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .100358317060817 3.3455e-08  
a 3.048780374629966 1.4569e-08 au
q 2.742809907144056 1.0338e-07 au
i 12.5072162512621 4.3367e-06 deg
node 196.2494077771552 1.7136e-05 deg
peri 95.04684892988784 2.8e-05 deg
M 244.24657321516 2.3928e-05 deg
tp 2459625.700034285230
(2022-Feb-15.20003429)
0.00013087 TDB
period 1944.409064977764
5.32
1.3937e-05
3.816e-08
d
yr
n .1851462259070043 1.3271e-09 deg/d
Q 3.354750842115877 1.6031e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2723  
   data-arc span      26179 days (71.67 yr)  
   first obs. used      1948-10-09  
   last obs. used      2020-06-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .44687  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-23 15:57:51  

Additional Information
 Earth MOID = 1.76415 au 
 Jupiter MOID = 1.87319 au 
 T_jup = 3.194 
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Orbital Elements at Epoch 2456738.5 (2014-Mar-22.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09828581439803578 3.3157e-08  
q 2.754590835730207 1.0214e-07 au
tp 2457673.300413278828
(2016-Oct-11.80041328)
0.00012968 TDB
node 196.4469746782189 1.7176e-05 deg
peri 93.23178589895804 2.8432e-05 deg
i 12.48195433090584 4.3294e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      2723  
   data-arc span      26179 days (71.67 yr)  
   first obs. used      1948-10-09  
   last obs. used      2020-06-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .44687  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-23 15:57:51  

Additional Information
 Jupiter MOID = 1.87319 au 
 T_jup = 3.194 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.099383737947321E-15 -3.357697346122642E-15 7.61991520788312E-13 3.129080709295784E-15 1.409868788442418E-13 5.50478277297282E-16
q -3.357697346122642E-15 1.043221042806312E-14 -1.776194193506892E-12 -6.875476386349627E-15 -3.544700119564696E-13 -3.855638393104396E-15
tp 7.61991520788312E-13 -1.776194193506892E-12 1.681772002475759E-8 2.198356895964676E-11 2.951242633923762E-9 4.452531351611018E-13
node 3.129080709295784E-15 -6.875476386349627E-15 2.198356895964676E-11 2.950231221855946E-10 -2.839012505610324E-10 -1.564589138907569E-11
peri 1.409868788442418E-13 -3.544700119564696E-13 2.951242633923762E-9 -2.839012505610324E-10 8.083728252082528E-10 1.553890744736254E-11
i 5.50478277297282E-16 -3.855638393104396E-15 4.452531351611018E-13 -1.564589138907569E-11 1.553890744736254E-11 1.874359084728888E-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 11.6   n/a MPO502186  
diameter diameter 18.595 km 0.071 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  
geometric albedo albedo 0.167   0.017 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  

3479 Malaparte (1980 TQ)          Discovered 1980-Oct-03 by Vavrova, Z. at Klet
Reference: DISCOVERY.DBLast Updated: 2003-08-29

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Alternate Designations
 1980 TQ = 1948 TD1 = 1957 JJ = 1957 JM = 1958 QB = 1969 RW = 1979 OL14 = 1980 TS10 = 1983 EK1 = 1985 SP 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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