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95128 (2002 AR152)
Classification: Main-belt Asteroid          SPK-ID: 2095128
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 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .02674467554376528 4.3581e-08  
a 2.720079048573403 1.8498e-08 au
q 2.647331416965913 1.1919e-07 au
i 6.463179700596647 5.7224e-06 deg
node 326.647740081209 3.9228e-05 deg
peri 250.6198191556717 0.00011 deg
M 316.6097865596369 0.00010287 deg
tp 2459197.996771484666
(2020-Dec-14.49677148)
0.00046838 TDB
period 1638.591564713096
4.49
1.6715e-05
4.576e-08
d
yr
n .2197008746734475 2.2412e-09 deg/d
Q 2.792826680180892 1.8993e-08 au
  Orbit Determination Parameters
   # obs. used (total)      605  
   data-arc span      8057 days (22.06 yr)  
   first obs. used      1998-04-01  
   last obs. used      2020-04-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5479  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 17:12:10  

Additional Information
 Earth MOID = 1.64901 au 
 Jupiter MOID = 2.20221 au 
 T_jup = 3.349 
[ show covariance matrix ]

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 15.4   n/a MPO432485  
diameter diameter 4.975 km 0.317 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.065   0.008 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

95128 (2002 AR152)          Discovered 2002-Jan-14 by LINEAR at Socorro
Reference: 20041028/Numbers.arcLast Updated: 2004-10-29

[ 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
2002-May-12 13:31 < 00:01 Juno 0.0251521892484178 0.0251504220657092 0.0251539564585118 7.80978164786083 7.80978158592652 2452407.063368537 0.432532095577298 106.370915271127 63.4220583472016 -44.2691540658849 48531.0271224132 T 18 CATAB v2.0f-lin.ifort 2020-May-20 17:12:27 2020-May-20 17:12
2050-Aug-31 15:16 < 00:01 Inter 0.0419709769804119 0.0419697102873868 0.0419722436750437 5.03148176194357 5.03148169262114 2470050.135882385 0.990427933433775 637.682557970435 63.1177645051714 -89.8855496702395 99420.0259965639 T 18 CATAB v2.0f-lin.ifort 2020-May-20 17:12:27 2020-May-20 17:12
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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