Skip Page Navigation
NASA JPL Caltech
NASA Logo - Jet Propulsion Laboratory + View the NASA Portal
+ Center for Near-Earth Object Studies
JPL Home Earth Solar System Stars & Galaxies Technology
JPL Solar System Dynamics
BODIES ORBITS EPHEMERIDES TOOLS PHYSICAL DATA DISCOVERY FAQ SITE MAP
JPL Small-Body Database Browser
Search: [ help ]  
(2019 NX1)
Classification: Apollo [NEO]          SPK-ID: 3843125
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6071001740591607 8.1571e-06  
a 2.576924016431645 5.3464e-05 au
q 1.012472997518762 1.762e-07 au
i 3.282979389005966 7.2302e-05 deg
node 280.0494634155588 3.3624e-05 deg
peri 14.14934216386322 0.0001483 deg
M 76.52472522698891 0.0023744 deg
tp 2458679.318793939938
(2019-Jul-14.81879394)
0.00010009 TDB
period 1510.952621373718
4.14
0.047022
0.0001287
d
yr
n .2382602835505839 7.4148e-06 deg/d
Q 4.141375035344529 8.5921e-05 au
  Orbit Determination Parameters
   # obs. used (total)      61  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      4 days  
   first obs. used      2019-07-04  
   last obs. used      2019-07-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .40768  
   source      ORB  
   producer      Giorgini  
   solution date      2019-Jul-16 14:11:12  

Additional Information
 Earth MOID = .0043971 au 
 Jupiter MOID = 1.10141 au 
 T_jup = 3.136 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458669.5 (2019-Jul-05.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6107041936765448 8.0847e-06  
q 1.012644447151998 1.6957e-07 au
tp 2458679.062057856523
(2019-Jul-14.56205786)
9.5449e-05 TDB
node 280.2735108020818 2.7533e-05 deg
peri 13.60992462687944 0.00013853 deg
i 3.46517301310391 6.824e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      61  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      4 days  
   first obs. used      2019-07-04  
   last obs. used      2019-07-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .40768  
   source      ORB  
   producer      Giorgini  
   solution date      2019-Jul-16 14:11:12  

Additional Information
 Jupiter MOID = 1.10141 au 
 T_jup = 3.136 
Orbit Covariance (6×6)
  e q tp node peri i
e 6.536212498408079E-11 -2.2370975631531E-13 -1.61880794249228E-10 -5.199723459853156E-11 6.757652520765912E-11 2.599890433234455E-10
q -2.2370975631531E-13 2.875237850345842E-14 -1.498215051354973E-11 3.712172151122787E-12 -2.306600889016225E-11 7.915819850950289E-12
tp -1.61880794249228E-10 -1.498215051354973E-11 9.11048489886896E-9 -1.886136130243398E-9 1.265551087504074E-8 -5.504335340247174E-9
node -5.199723459853156E-11 3.712172151122787E-12 -1.886136130243398E-9 7.580906514038774E-10 -3.265671984633372E-9 1.304912862255332E-9
peri 6.757652520765912E-11 -2.306600889016225E-11 1.265551087504074E-8 -3.265671984633372E-9 1.919074047688336E-8 -7.283053709602642E-9
i 2.599890433234455E-10 7.915819850950289E-12 -5.504335340247174E-9 1.304912862255332E-9 -7.283053709602642E-9 4.6567230822897E-9

Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 27.7   .33365 MPO473709 autocmod 2.7

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Jul-09 11:22 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin