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(2015 VE66)
Classification:
Apollo
[
NEO
]
SPK-ID:
3734183
[
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 36
(heliocentric ecliptic J2000)
Element
Value
Uncertainty (1-sigma)
Units
e
.4997325044139038
4.6527e-05
a
2.011030845648281
0.00018879
au
q
1.006053364698855
8.7677e-07
au
i
6.116689911884359
0.00042647
deg
node
238.2928594818757
8.7102e-06
deg
peri
187.5207081947167
0.00023737
deg
M
346.1591780556402
0.098874
deg
t
p
2459436.548467846419
(2021-Aug-10.04846785)
0.29173
TDB
period
1041.661288807061
2.85
0.14668
0.0004016
d
yr
n
.3456017842539602
4.8665e-05
deg/d
Q
3.016008326597707
0.00028313
au
Orbit Determination Parameters
# obs. used (total)
259
data-arc span
82 days
first obs. used
2015-11-09
last obs. used
2016-01-30
planetary ephem.
DE441
SB-pert. ephem.
SB441-N16
condition code
6
norm. resid. RMS
.3528
source
ORB
producer
Otto Matic
solution date
2021-Apr-15 15:13:32
Additional Information
Earth MOID
= .0204802 au
Jupiter MOID
= 2.3283 au
T_jup
= 3.658
[ show covariance matrix ]
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Ephemeris
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Orbit Diagram
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Orbital Elements
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Physical Parameter Table
Parameter
Symbol
Value
Units
Sigma
Reference
Notes
absolute magnitude
H
24.1
n/a
E2016A09
rotation period
rot_per
0.037
h
n/a
LCDB (Rev. 2020-October); Warner et al., 2009
Published Reference List:
[Thirouin, A.; Moskovitz, N.A.; Binzel, R.P.; Christensen, E.J.; et al. (2018) Astrophys. J. Supp. Series 2391, A4.]
[ show close-approach data ]
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Ephemeris
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Orbital Elements
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Physical Parameters
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Close-Approach Data
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2021-Jul-29 10:19 UT
(server date/time)
Site Manager:
Ryan S. Park
Webmaster
:
Alan B. Chamberlin
