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101058 (1998 RN3)
Classification: Mars-crossing Asteroid          SPK-ID: 2101058
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5158582584538565 6.2714e-08  
a 3.137398040266495 2.5503e-08 au
q 1.518945351138079 2.0381e-07 au
i 21.17755061421855 9.3661e-06 deg
node 348.2374444334807 1.9965e-05 deg
peri 84.32274928959913 2.1832e-05 deg
M 289.5175409481981 5.0049e-06 deg
tp 2459397.903241510754
(2021-Jul-02.40324151)
3.0109e-05 TDB
period 2029.798177710059
5.56
2.4749e-05
6.776e-08
d
yr
n .177357534336807 2.1625e-09 deg/d
Q 4.755850729394911 3.8659e-08 au
  Orbit Determination Parameters
   # obs. used (total)      506  
   data-arc span      9713 days (26.59 yr)  
   first obs. used      1994-02-08  
   last obs. used      2020-09-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .45741  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 20:02:40  

Additional Information
 Earth MOID = .692498 au 
 Jupiter MOID = 1.85121 au 
 T_jup = 2.899 
[ 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 MPO351567  
diameter diameter 4.692 km 0.918 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2016AJ....152...63N)  
geometric albedo albedo 0.055   0.025 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2016AJ....152...63N)  

101058 (1998 RN3)          Discovered 1998-Sep-14 by LINEAR at Socorro
Reference: 20051019/Numbers.arcLast Updated: 2005-10-26

[ show close-approach data ]
Alternate Designations
 1998 RN3 = 1994 CE15 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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