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JPL Small-Body Database Browser
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(2019 TP5)
Classification: Apollo [NEO]          SPK-ID: 3878621
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 2458766.5 (2019-Oct-10.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .662452336454921 0.0012164  
a 1.895253860521628 0.0056504 au
q .6397385124438666 0.00039819 au
i 8.789567784604131 0.015335 deg
node 204.9867016213026 0.0020411 deg
peri 262.1375160571256 0.00047699 deg
M 339.1531879905791 0.10773 deg
tp 2458821.686984104186
(2019-Dec-04.18698410)
0.038384 TDB
period 953.0145073754526
2.61
4.2619
0.01167
d
yr
n .3777487091895583 0.0016893 deg/d
Q 3.150769208599389 0.0093935 au
  Orbit Determination Parameters
   # obs. used (total)      41  
   data-arc span      10 days  
   first obs. used      2019-10-07  
   last obs. used      2019-10-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .47615  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-04 07:20:13  

Additional Information
 Earth MOID = .00532144 au 
 Jupiter MOID = 2.11461 au 
 T_jup = 3.639 
[ 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 25.042   .63711 5 autocmod 2.8

[ 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
1910-Mar-31 14:58 7_09:22 Earth 0.0479862715172268 0.0463765676926359 0.138805355256501 18.728118349419 18.7251532750878 2418762.123391977 10641.6073821888 5909970.29105818 133.540489901308 -75.1299136143243 53666.6752767059 T 5 CATAB v2.0f-lin.ifort 2019-Dec-04 07:20:16 2019-Dec-04 07:20
2019-Oct-18 07:38 < 00:01 Earth 0.021021107783912 0.0209059870322857 0.0211362276085353 18.5641157269821 18.5572866441764 2458774.818270453 0.0577865514801086 5736.35976687957 4.23740131040735 0.032504350709359 432.39424625495 T 5 CATAB v2.0f-lin.ifort 2019-Dec-04 07:20:16 2019-Dec-04 07:20
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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