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85046 (6126 P-L)
Classification: Main-belt Asteroid          SPK-ID: 2085046
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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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 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1961676993130697 4.3524e-08  
a 2.309555912809803 7.8263e-09 au
q 1.856495642959007 1.0005e-07 au
i 6.058883291694001 4.7998e-06 deg
node 3.251803679799562 4.1765e-05 deg
peri 10.74239617192089 4.3409e-05 deg
M 49.89424823068047 1.2744e-05 deg
tp 2459022.819760669705
(2020-Jun-22.31976067)
4.5101e-05 TDB
period 1282.009218039956
3.51
6.5164e-06
1.784e-08
d
yr
n .2808092133303055 1.4273e-09 deg/d
Q 2.762616182660599 9.3616e-09 au
  Orbit Determination Parameters
   # obs. used (total)      622  
   data-arc span      22030 days (60.31 yr)  
   first obs. used      1960-09-24  
   last obs. used      2021-01-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50575  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 07:39:24  

Additional Information
 Earth MOID = .855935 au 
 Jupiter MOID = 2.70609 au 
 T_jup = 3.552 
[ 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 16.0   n/a MPO436370  

85046 (6126 P-L)          Discovered 1960-Sep-24 by van Houten, C. J., van Houten-Groeneveld, I., Gehrels, T. at Palomar
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

[ 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
2001-Jul-03 19:46 < 00:01 Amphi 0.0497942168279192 0.0497919333827788 0.0497965002756866 2.54667567607923 2.5466756307456 2452094.323530358 0.97339517102217 120.017427028994 100.226165329657 -35.4637938644112 66361.5710149169 T 13 CATAB v2.0f-lin.ifort 2021-Feb-24 07:39:26 2021-Feb-24 07:39
2049-Jul-20 08:09 00:01 Amphi 0.0450866231310285 0.0450835049175269 0.0450897414075967 2.47692929245667 2.47692924097985 2469642.839371382 1.05102870309875 181.575588751257 69.6342143937135 -34.104057146915 62331.2206175821 T 13 CATAB v2.0f-lin.ifort 2021-Feb-24 07:39:26 2021-Feb-24 07:39

Alternate Designations
 6126 P-L = 1999 XQ200 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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