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 ]  
(2015 FW33)
Classification: Apollo [NEO]          SPK-ID: 3713939
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2189469123991602 0.00016451  
a 1.301102276916964 0.00028965 au
q 1.016229950670478 1.2186e-05 au
i 7.221264815701674 0.005016 deg
node 178.0769746369818 0.0016671 deg
peri .5237979425829118 0.0058537 deg
M 180.1330128105206 0.44847 deg
tp 2459271.341082933860
(2021-Feb-25.84108293)
0.76574 TDB
period 542.0827433634386
1.48
0.18102
0.0004956
d
yr
n .6641052577440905 0.00022177 deg/d
Q 1.585974603163451 0.00035307 au
  Orbit Determination Parameters
   # obs. used (total)      48  
   data-arc span      12 days  
   first obs. used      2015-03-19  
   last obs. used      2015-03-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48883  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:59  

Additional Information
 Earth MOID = .0203996 au 
 Jupiter MOID = 3.37328 au 
 T_jup = 4.967 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457102.5 (2015-Mar-21.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2190955465425889 0.00018108  
q 1.016128706930105 1.5074e-05 au
tp 2457101.870916281301
(2015-Mar-20.37091628)
0.0035441 TDB
node 178.2258549534497 0.00064831 deg
peri .09327362288768548 0.003765 deg
i 7.259586473814899 0.0048784 deg
  Orbit Determination Parameters
   # obs. used (total)      48  
   data-arc span      12 days  
   first obs. used      2015-03-19  
   last obs. used      2015-03-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48883  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:59  

Additional Information
 Jupiter MOID = 3.37328 au 
 T_jup = 4.967 
Orbit Covariance (6×6)
  e q tp node peri i
e 3.278933488162982E-8 2.729489532741732E-9 6.410304940580002E-7 -1.173895764851603E-7 6.810023404953048E-7 8.833423210744867E-7
q 2.729489532741732E-9 2.272128812417183E-10 5.336034546482329E-8 -9.771983069614719E-9 5.668771131310383E-8 7.35328952185301E-8
tp 6.410304940580002E-7 5.336034546482329E-8 1.256055988824607E-5 -2.294759697488543E-6 1.334360941852612E-5 1.726414241081886E-5
node -1.173895764851603E-7 -9.771983069614719E-9 -2.294759697488543E-6 4.203098495412847E-7 -2.437889720288079E-6 -3.162511425436945E-6
peri 6.810023404953048E-7 5.668771131310383E-8 1.334360941852612E-5 -2.437889720288079E-6 1.417551401503186E-5 1.834068077389317E-5
i 8.833423210744867E-7 7.35328952185301E-8 1.726414241081886E-5 -3.162511425436945E-6 1.834068077389317E-5 2.379844463865797E-5

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 25.8   n/a MPO339523  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Aug-10 00:34 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin