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95546 (2002 EE88)
Classification: Main-belt Asteroid          SPK-ID: 2095546
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05457819656732815 3.9578e-08  
a 2.856020360835455 1.7884e-08 au
q 2.700143920181486 1.1796e-07 au
i 3.051595593979997 4.4829e-06 deg
node 68.69761464015735 7.135e-05 deg
peri 6.872777514966812 8.2271e-05 deg
M 24.40409671082709 3.9202e-05 deg
tp 2458880.991000020091
(2020-Feb-01.49100002)
0.00019204 TDB
period 1762.951544675682
4.83
1.6559e-05
4.534e-08
d
yr
n .204203003246029 1.918e-09 deg/d
Q 3.011896801489424 1.886e-08 au
  Orbit Determination Parameters
   # obs. used (total)      736  
   data-arc span      9300 days (25.46 yr)  
   first obs. used      1994-08-12  
   last obs. used      2020-01-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59137  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 23:46:49  

Additional Information
 Earth MOID = 1.7152 au 
 Jupiter MOID = 2.12932 au 
 T_jup = 3.299 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457175.5 (2015-Jun-02.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05172549562438059 3.9418e-08  
q 2.707474792869611 1.1707e-07 au
tp 2457118.280977840321
(2015-Apr-05.78097784)
0.00020616 TDB
node 68.77965040208315 7.1425e-05 deg
peri 6.912213429161022 8.3617e-05 deg
i 3.050695350356322 4.4786e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      736  
   data-arc span      9300 days (25.46 yr)  
   first obs. used      1994-08-12  
   last obs. used      2020-01-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59137  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 23:46:49  

Additional Information
 Jupiter MOID = 2.12932 au 
 T_jup = 3.299 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.553769817411712E-15 -4.568526631178501E-15 -8.779267099120482E-13 -2.737963430508154E-15 -1.723116541464606E-13 -5.875167488011268E-16
q -4.568526631178501E-15 1.370604092898173E-14 1.967083389662E-12 6.429755396393607E-15 3.793302572649674E-13 2.020661467973987E-15
tp -8.779267099120482E-13 1.967083389662E-12 4.250367149942872E-8 1.725289773327404E-11 8.97825234240374E-9 -8.091508726038732E-13
node -2.737963430508154E-15 6.429755396393607E-15 1.725289773327404E-11 5.101559757711713E-9 -5.090487793096612E-9 -4.037111404928432E-11
peri -1.723116541464606E-13 3.793302572649674E-13 8.97825234240374E-9 -5.090487793096612E-9 6.99183204029506E-9 4.014404755149286E-11
i -5.875167488011268E-16 2.020661467973987E-15 -8.091508726038732E-13 -4.037111404928432E-11 4.014404755149286E-11 2.005805029914296E-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 15.2   n/a MPO412721  

95546 (2002 EE88)          Discovered 2002-Mar-09 by LINEAR at Socorro
Reference: 20041028/Numbers.arcLast Updated: 2004-10-29

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