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183863 (2004 CE14)
Classification: Main-belt Asteroid          SPK-ID: 2183863
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1115263723053775 4.0909e-08  
a 2.409619905888609 1.2511e-08 au
q 2.140883739150027 9.9794e-08 au
i 7.922722138005801 5.2452e-06 deg
node 141.8962943081573 3.0332e-05 deg
peri 337.463084395677 3.8087e-05 deg
M 204.6048793775984 2.195e-05 deg
tp 2459790.233932724831
(2022-Jul-29.73393272)
8.3828e-05 TDB
period 1366.221892493152
3.74
1.064e-05
2.913e-08
d
yr
n .2635003889031917 2.0521e-09 deg/d
Q 2.678356072627191 1.3906e-08 au
  Orbit Determination Parameters
   # obs. used (total)      395  
   data-arc span      7051 days (19.30 yr)  
   first obs. used      2000-01-07  
   last obs. used      2019-04-28  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .54141  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 21:40:43  

Additional Information
 Earth MOID = 1.15876 au 
 Jupiter MOID = 2.38182 au 
 T_jup = 3.499 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457134.5 (2015-Apr-22.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1125387808428582 4.0748e-08  
q 2.13783690816216 9.9528e-08 au
tp 2457057.414530790887
(2015-Feb-03.91453079)
8.2157e-05 TDB
node 141.9575575827854 3.0384e-05 deg
peri 337.0157019351556 3.7969e-05 deg
i 7.916265759306116 5.241e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      395  
   data-arc span      7051 days (19.30 yr)  
   first obs. used      2000-01-07  
   last obs. used      2019-04-28  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .54141  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 21:40:43  

Additional Information
 Jupiter MOID = 2.38182 au 
 T_jup = 3.499 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.660359164439251E-15 -4.031305010671183E-15 1.063020692414026E-12 -1.395017259571667E-14 2.964812481342289E-13 -1.161760564086176E-15
q -4.031305010671183E-15 9.90580015230429E-15 -2.644575638993522E-12 3.225645413140365E-14 -7.362136977864983E-13 3.239782785858561E-15
tp 1.063020692414026E-12 -2.644575638993522E-12 6.749692221284069E-9 -3.731000183275373E-11 1.885649306947594E-9 -4.751369944338982E-12
node -1.395017259571667E-14 3.225645413140365E-14 -3.731000183275373E-11 9.231818823210082E-10 -9.239463376221601E-10 3.578342176660279E-11
peri 2.964812481342289E-13 -7.362136977864983E-13 1.885649306947594E-9 -9.239463376221601E-10 1.441632606082901E-9 -3.669325845953263E-11
i -1.161760564086176E-15 3.239782785858561E-15 -4.751369944338982E-12 3.578342176660279E-11 -3.669325845953263E-11 2.746764277654227E-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 16.56   n/a MPCxxxxx  

183863 (2004 CE14)          Discovered 2004-Feb-11 by LONEOS at Anderson Mesa
Reference: 20080420/Numbers.arcLast Updated: 2008-04-23

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2039-Aug-29 08:19 00:05 Psych 0.0187330093468235 0.0187295861688833 0.0187364337188055 2.56001618514694 2.56001593285526 2466029.846868880 4.80534011225883 298.314390730616 47.3017443566169 -56.2562833550385 49429.7121047709 T 16 CATAB v2.0f-lin.ifort 2021-Apr-13 21:40:44 2021-Apr-13 21:40
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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