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89282 Suzieimber (2001 VD17)
Classification: Main-belt Asteroid          SPK-ID: 2089282
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 .1719439603661602 5.0998e-08  
a 2.555566135622986 1.4895e-08 au
q 2.116151973286326 1.3293e-07 au
i 4.904997125782325 5.1239e-06 deg
node 144.9109617737165 5.9464e-05 deg
peri 188.064691873021 6.0939e-05 deg
M 252.2314047158219 1.3998e-05 deg
tp 2459447.202964885457
(2021-Aug-20.70296489)
5.8866e-05 TDB
period 1492.20714007371
4.09
1.3046e-05
3.572e-08
d
yr
n .2412533691416443 2.1092e-09 deg/d
Q 2.994980297959646 1.7456e-08 au
  Orbit Determination Parameters
   # obs. used (total)      546  
   data-arc span      7262 days (19.88 yr)  
   first obs. used      2000-06-09  
   last obs. used      2020-04-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55808  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 20:47:25  

Additional Information
 Earth MOID = 1.1059 au 
 Jupiter MOID = 2.36795 au 
 T_jup = 3.412 
[ 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 16.3   n/a MPO436398  

89282 Suzieimber           Discovered 2001 Nov. 10 by P. Pravec and P. Kusnirak at Ondrejov.
Suzie Imber (b. 1983) is a planetary scientist, an accomplished mountaineer, elite sportswoman, and TV personality. She is a direct and powerful inspiration for the next generation through her extensive STEM outreach activities, presenting to many thousands of school children about space exploration.
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character)
Reference: MPC batch dated 2018-10-26Last Updated: 2019-04-09

[ 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
2085-Jul-03 02:03 < 00:01 Juno 0.00774408598293134 0.00773090013970019 0.0077572961222709 6.18114631983217 6.18114606567241 2482774.585727525 0.820600541516266 950.493005381782 53.9059553015133 46.2970705223438 15550.9147361968 T 18 CATAB v2.0f-lin.ifort 2020-Nov-12 20:47:26 2020-Nov-12 20:47
2172-Oct-23 21:30 00:06 Hebe 0.004589262006207 0.00454180771865002 0.00463680702140448 4.46362128973888 4.46362098626078 2514663.396137455 5.72660287197965 2576.67840175424 45.6567551176108 -23.2536708512722 5936.70236893129 T 18 CATAB v2.0f-lin.ifort 2020-Nov-12 20:47:26 2020-Nov-12 20:47

Alternate Designations
 2001 VD17 = 2003 BE45 = 2003 BQ85 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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