C/2017 T1 Heinze
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Comet C/2017 T1 was discovered on 2 October 2017 by Aren Heinze (Asteroid Terrestrial-impact Last Alert System (ATLAS) search program), that is about 4.7 months before its perihelion passage. Next, pre-discovery data were found going back to September 28. Comet was observed extensively before perihelion passage and notable less frequently after perihelion until 25 March 2018. At the endof data arc is a series of three measurements from June 18, preceded by a 2.7-month break in the data. C/2017 T1 had closest approach to the Earth on 4 January 2018 (0.222 au, 17 days before the perihelion passage).

This is a comet with NG effects strongly manifested in positional data fitting and during GR orbit determination the series of three measurements from June 17 were ejected due to large residuals and systematically small weights were obtained for all remaining post-perihelion observations. Therefore, this GR orbit (solutions 'a5') is based on data spanning over 0.488 yr in a range of heliocentric distances: 2.60 au – 0.581 au (perihelion) – 0.90 au. During NG orbit determination weights in post-perihelion leg are also systematically small; however, series of last three measurements were not ejected. So, NG orbit ('n5') is based on data spanning over 0.718 yr in a range of heliocentric distances: 2.60 au – 0.581 au (perihelion) – 2.18 au. However, we suggest the solution 'pn' (based on the pre-perihelion orbital leg up to heliocentric distance of 0.782 au) to be treated as 'preferred' orbit for the study of the origin of this comet.

Only solution 'n1' suggest that this is an Oort spike comet; all remaining (including the 'preferred orbit') give similar values for original semimajor axis, that is from 3560 au to 4050 au (uncertainty of one sigma is applied). According to solutions 'a5' and 'n5' this comet suffers small planetary perturbations while passing through the planetary system; these perturbations lead to a sligthy more tight orbit after passage through the planetary zone (see future barycentric orbits).

See also: Sekanina 2019.
solution description
number of observations 1016
data interval 2017 09 28 – 2018 01 28
data arc selection data generally limited to pre-perihelion (PRE)
range of heliocentric distances 2.6 au – 0.782au
type of model of motion NS - non-gravitational orbits for standard g(r)
data weighting YES
number of residuals 2015
RMS [arcseconds] 0.55
orbit quality class 2b
orbital elements (heliocentric ecliptic J2000)
Epoch 2018 03 23
perihelion date 2018 02 21.71430957 ± 0.00047886
perihelion distance [au] 0.58036897 ± 0.00002742
eccentricity 0.99859413 ± 0.00017581
argument of perihelion [°] 96.912468 ± 0.000931
ascending node [°] 102.295999 ± 0.002202
inclination [°] 96.823408 ± 0.001003
reciprocal semi-major axis [10-6 au-1] 2,422.38 ± 302.96
Upper panel: Time distribution of positional observations with corresponding heliocentric (red curve) and geocentric (green curve) distance at which they were taken. The horizontal dotted line shows the perihelion distance for a given comet whereas vertical dotted line — the moment of perihelion passage.
Middle panel(s): O-C diagram for a given solution (sometimes in comparison to another solution available in CODE), where residuals in right ascension are shown using magenta dots and in declination by blue open circles.
Lowest panel: Relative weights for a given data set(s).
non-gravitational parameters
A1 [10-8au/day2] 8.3843 ± 0.7381
A2 [10-8au/day2] -7.6569 ± 0.8291
A3 [10-8au/day2] -8.0364 ± 0.899
m -2.15
n 5.093
k -4.6142
r0 [au] 2.808
α 0.1113