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3396 Muazzez (A915 TE)
Classification: Outer Main-belt Asteroid          SPK-ID: 2003396
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 40 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1809433236567357 3.9018e-08  
a 3.397931370230744 1.9231e-08 au
q 2.783098374543707 1.3965e-07 au
i 8.318157399181473 3.6641e-06 deg
node 37.91720774425705 2.6194e-05 deg
peri 315.3536321680776 2.788e-05 deg
M 316.1184918621982 1.0051e-05 deg
tp 2459279.368445442779
(2021-Mar-05.86844544)
6.4653e-05 TDB
period 2287.811987777083
6.26
1.9422e-05
5.317e-08
d
yr
n .1573555877508048 1.3359e-09 deg/d
Q 4.012764365917781 2.2711e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2752  
   data-arc span      38366 days (105.04 yr)  
   first obs. used      1915-10-15  
   last obs. used      2020-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .42682  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-13 04:00:38  

Additional Information
 Earth MOID = 1.78649 au 
 Jupiter MOID = 1.48137 au 
 T_jup = 3.104 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457232.5 (2015-Jul-29.0) TDB
Reference: JPL 40 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1850230218232533 3.8713e-08  
q 2.759814218310921 1.3844e-07 au
tp 2457006.340822365300
(2014-Dec-14.84082237)
6.0995e-05 TDB
node 38.06710393678194 2.6083e-05 deg
peri 316.329491119432 2.7698e-05 deg
i 8.349280417243241 3.6758e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      2752  
   data-arc span      38366 days (105.04 yr)  
   first obs. used      1915-10-15  
   last obs. used      2020-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .42682  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-13 04:00:38  

Additional Information
 Jupiter MOID = 1.48137 au 
 T_jup = 3.104 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.498703890143299E-15 -5.332165267875341E-15 -3.124000170586336E-13 3.483622801330958E-15 -2.623249945147363E-14 -1.79037646273741E-15
q -5.332165267875341E-15 1.916546968535186E-14 1.032238766282445E-12 -1.591076490818804E-14 8.809027772178098E-14 6.911613345919011E-15
tp -3.124000170586336E-13 1.032238766282445E-12 3.720431476423967E-9 -1.678376706069715E-12 5.896815680650838E-10 2.186030872245947E-12
node 3.483622801330958E-15 -1.591076490818804E-14 -1.678376706069715E-12 6.803295370848822E-10 -6.734242155562862E-10 -1.059798188934883E-11
peri -2.623249945147363E-14 8.809027772178098E-14 5.896815680650838E-10 -6.734242155562862E-10 7.67186635608499E-10 1.08218157487601E-11
i -1.79037646273741E-15 6.911613345919011E-15 2.186030872245947E-12 -1.059798188934883E-11 1.08218157487601E-11 1.351178760956296E-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 11.0   n/a MPO350828  
diameter diameter 32.519 km 0.182 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  
geometric albedo albedo 0.072   0.009 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  

3396 Muazzez (A915 TE)          Discovered 1915-Oct-15 by Wolf, M. at Heidelberg
Reference: DISCOVERY.DBLast Updated: 2003-08-29

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Alternate Designations
 A915 TE = 1940 TL = 1957 HO = 1971 SL1 = 1973 AJ = 2019 FE5 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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