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(2015 BE92)
Classification: Aten [NEO]          SPK-ID: 3704767
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1973128482737253 1.713e-06  
a .9732291975089145 3.0141e-07 au
q .7811985725252786 1.4963e-06 au
i 1.042217421432823 7.3843e-06 deg
node 290.1402755185192 8.4282e-05 deg
peri 303.2032961854923 0.00011537 deg
M 323.0233640055541 0.00088284 deg
tp 2459236.520191589601
(2021-Jan-22.02019159)
0.00087662 TDB
period 350.6881743975838
0.96
0.00016292
4.461e-07
d
yr
n 1.026553007150618 4.7689e-07 deg/d
Q 1.16525982249255 3.6089e-07 au
  Orbit Determination Parameters
   # obs. used (total)      76  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      14 days  
   first obs. used      2015-01-14  
   last obs. used      2015-01-28  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      3  
   norm. resid. RMS      .42032  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 12:30:29  

Additional Information
 Earth MOID = .00562807 au 
 Jupiter MOID = 3.81856 au 
 T_jup = 6.194 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457041.5 (2015-Jan-19.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1980493616867124 1.7167e-06  
q .777291411271354 1.4484e-06 au
tp 2457132.755194730852
(2015-Apr-20.25519473)
0.00021092 TDB
node 292.4315637186039 7.3662e-05 deg
peri 302.2559474824599 0.00010886 deg
i 1.176409292331041 7.4291e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      76  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      14 days  
   first obs. used      2015-01-14  
   last obs. used      2015-01-28  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      3  
   norm. resid. RMS      .42032  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 12:30:29  

Additional Information
 Jupiter MOID = 3.81856 au 
 T_jup = 6.194 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.947173411244237E-12 -2.466770493856352E-12 -3.553672213156536E-10 -6.23814565077409E-11 -1.899570099081169E-11 8.869284110512853E-13
q -2.466770493856352E-12 2.097858118646457E-12 2.900956850668576E-10 5.654887906745416E-11 -5.659457278598055E-13 -7.440245614876478E-14
tp -3.553672213156536E-10 2.900956850668576E-10 4.448770399122564E-8 6.550247446275375E-9 5.95849618699604E-9 -2.561750591908197E-10
node -6.23814565077409E-11 5.654887906745416E-11 6.550247446275375E-9 5.426066651214759E-9 -5.292306536570756E-9 4.288333583537104E-10
peri -1.899570099081169E-11 -5.659457278598055E-13 5.95849618699604E-9 -5.292306536570756E-9 1.185040919751469E-8 -6.978230047172153E-10
i 8.869284110512853E-13 -7.440245614876478E-14 -2.561750591908197E-10 4.288333583537104E-10 -6.978230047172153E-10 5.519122664073249E-11

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 28.1   n/a MPO331391  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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