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(2012 VU76)
Classification: Apollo [NEO]          SPK-ID: 3617715
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .128503289445039 1.4494e-06  
a 1.018632063039575 2.3981e-07 au
q .8877344922048029 1.2674e-06 au
i 6.75640899701258 6.0337e-05 deg
node 52.34854228110959 2.4218e-05 deg
peri 88.28842115907068 0.00011734 deg
M 68.7335175203816 0.0011113 deg
tp 2459324.804729217256
(2021-Apr-20.30472922)
0.0011339 TDB
period 375.5125361383459
1.03
0.00013261
3.631e-07
d
yr
n .9586896983576848 3.3855e-07 deg/d
Q 1.149529633874346 2.7063e-07 au
  Orbit Determination Parameters
   # obs. used (total)      47  
   data-arc span      596 days (1.63 yr)  
   first obs. used      2012-11-13  
   last obs. used      2014-07-02  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      2  
   norm. resid. RMS      .34466  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:13:25  

Additional Information
 Earth MOID = .00319657 au 
 Jupiter MOID = 3.84527 au 
 T_jup = 5.980 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456565.5 (2013-Sep-30.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1281848014177885 1.4498e-06  
q .8878281655546714 1.2306e-06 au
tp 2456697.848582298332
(2014-Feb-09.34858230)
0.00013368 TDB
node 52.63745296050518 1.5591e-05 deg
peri 88.78457572833273 0.00011511 deg
i 6.760083997133401 6.0303e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      47  
   data-arc span      596 days (1.63 yr)  
   first obs. used      2012-11-13  
   last obs. used      2014-07-02  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      2  
   norm. resid. RMS      .34466  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:13:25  

Additional Information
 Jupiter MOID = 3.84527 au 
 T_jup = 5.980 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.101983121055555E-12 -1.784003416419966E-12 1.92803633459359E-10 1.98960654119859E-11 1.654969553822182E-10 8.637648137919015E-11
q -1.784003416419966E-12 1.514277176990036E-12 -1.635256113407763E-10 -1.689884242326469E-11 -1.404283909965164E-10 -7.333805040895866E-11
tp 1.92803633459359E-10 -1.635256113407763E-10 1.787146356729432E-8 1.819285089213817E-9 1.532989792094408E-8 7.930412312848201E-9
node 1.98960654119859E-11 -1.689884242326469E-11 1.819285089213817E-9 2.430906152597015E-10 1.513031068816797E-9 8.419356238957872E-10
peri 1.654969553822182E-10 -1.404283909965164E-10 1.532989792094408E-8 1.513031068816797E-9 1.3249341717756E-8 6.81105047251136E-9
i 8.637648137919015E-11 -7.333805040895866E-11 7.930412312848201E-9 8.419356238957872E-10 6.81105047251136E-9 3.63651199224937E-9

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 25.7   n/a MPO244152  

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