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180849 (2005 GX152)
Classification: Main-belt Asteroid          SPK-ID: 2180849
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08969820263216238 3.2246e-08  
a 2.323205130000567 1.1572e-08 au
q 2.114817805493697 7.2588e-08 au
i 6.643244198356822 5.8495e-06 deg
node 186.6262403125325 2.8444e-05 deg
peri 74.66988687133095 4.5902e-05 deg
M 110.3723886164482 3.6538e-05 deg
tp 2458803.959358777995
(2019-Nov-16.45935878)
0.00013103 TDB
period 1293.390789393934
3.54
9.6636e-06
2.646e-08
d
yr
n .2783381503502831 2.0796e-09 deg/d
Q 2.531592454507438 1.261e-08 au
  Orbit Determination Parameters
   # obs. used (total)      315  
   data-arc span      8295 days (22.71 yr)  
   first obs. used      1998-04-22  
   last obs. used      2021-01-06  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .54165  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 21:28:12  

Additional Information
 Earth MOID = 1.10987 au 
 Jupiter MOID = 2.51015 au 
 T_jup = 3.562 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458028.5 (2017-Oct-02.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08924891045192722 3.2207e-08  
q 2.116590785702062 7.2468e-08 au
tp 2457511.367968753339
(2016-May-02.86796875)
0.00013153 TDB
node 186.6755697037662 2.8442e-05 deg
peri 75.04431982296937 4.6044e-05 deg
i 6.642642574249761 5.849e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      315  
   data-arc span      8295 days (22.71 yr)  
   first obs. used      1998-04-22  
   last obs. used      2021-01-06  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .54165  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 21:28:12  

Additional Information
 Jupiter MOID = 2.51015 au 
 T_jup = 3.562 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.037283087758675E-15 -2.311181782963185E-15 -7.632496870258162E-13 2.015880433416078E-15 -2.256466245174978E-13 2.573940429170465E-15
q -2.311181782963185E-15 5.251640929316798E-15 1.752959676296647E-12 -5.72130878373016E-15 5.273558975543499E-13 -5.599428052670665E-15
tp -7.632496870258162E-13 1.752959676296647E-12 1.72999972470933E-8 -6.446016905118836E-11 4.766684156339152E-9 -3.902989579770445E-12
node 2.015880433416078E-15 -5.72130878373016E-15 -6.446016905118836E-11 8.089420625807244E-10 -8.205893122030821E-10 -6.407339083092846E-12
peri -2.256466245174978E-13 5.273558975543499E-13 4.766684156339152E-9 -8.205893122030821E-10 2.120040610365803E-9 5.272906687723174E-12
i 2.573940429170465E-15 -5.599428052670665E-15 -3.902989579770445E-12 -6.407339083092846E-12 5.272906687723174E-12 3.421076620448457E-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 17.19   n/a MPCxxxxx  

180849 (2005 GX152)          Discovered 2005-Apr-13 by LONEOS at Anderson Mesa
Reference: 20080321/Numbers.arcLast Updated: 2008-03-26

[ 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
2128-Aug-20 05:01 < 00:01 Juno 0.0405500984213794 0.0405443334861581 0.0405558818719372 6.72164408474239 6.72164404010707 2498527.708696130 0.535647425531202 1455.29707365602 83.0551807773618 79.0676516843088 71691.0458381842 T 17 CATAB v2.0f-lin.ifort 2021-Apr-13 21:28:13 2021-Apr-13 21:28
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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