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(2004 TG10)
Classification: Apollo [NEO, PHA]          SPK-ID: 3256324
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .8618441028987675 8.4059e-08  
a 2.23337971972461 1.997e-08 au
q .3085545787462529 1.8966e-07 au
i 4.181102736715494 2.5072e-05 deg
node 205.0870118253788 0.00012044 deg
peri 317.3675684113326 0.00011874 deg
M 213.3681299720307 1.0199e-05 deg
tp 2459497.055905919589
(2021-Oct-09.55590592)
3.6952e-05 TDB
period 1219.108275008389
3.34
1.6351e-05
4.477e-08
d
yr
n .2952978069134366 3.9607e-09 deg/d
Q 4.158204860702968 3.7181e-08 au
  Orbit Determination Parameters
   # obs. used (total)      93  
   data-arc span      5040 days (13.80 yr)  
   first obs. used      2004-10-05  
   last obs. used      2018-07-24  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54787  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Jul-24 06:22:25  

Additional Information
 Earth MOID = .0224973 au 
 Jupiter MOID = .885636 au 
 T_jup = 2.993 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 19.4   n/a MPO315194  
diameter diameter 1.316 km 0.605 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  
geometric albedo albedo 0.018   0.037 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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