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Re: HALE-BOPP vs 12TH PLANET


Article: <5d0ek4$2bs@dfw-ixnews9.ix.netcom.com>
From: saquo@ix.netcom.com(Nancy )
Subject: Re: HALE-BOPP vs 12TH PLANET
Date: 1 Feb 1997 22:03:48 GMT

In article <5cpaol$l4u@news.Hawaii.Edu> David Tholen demands:
>>>> I ran these orbital elements into my Skymap program and see that
>>>> NASA has indeed moved the perihelion placement AWAY from occulting
>>>> Gamma Andromedae. I note with amusement that this only occurred
>>>> AFTER the Zetas called them on this occultation maneuver.
>>>
>>> Balderdash. Please reproduce any set of orbital elements from
>>> the past year that shows any occultation with this star. Be sure
>>> to provide the source.
>>
>> The source is NASA, JPL, and the IAU.
>
> I don't want your web site as a source of orbital elements that
> show an occultation. I want the alleged NASA or JPL or IAU
> source.
> tholen@galileo.ifa.hawaii.edu

Well that's what my web site on Hale-Bopp SHOWS, but as I guess you're lazy as well unable to do anything but nit-pick, I've plopped a partial copy below.

........

COMET COMMENTS by Don Marchholz, 12 Sept 1995 00:13:21 GMT

Two new comets have been discovered recently, one should be visible in our morning sky soon. Meanwhile, Comet Hale-Bopp continues to lookpromising.

THE POSITION OF HALE-BOPP THROUGH 1997

Below is a table giving information about Comet Hale-Bopp through 1997. The date is followed by Right Ascension and Declination in 2000 coordinates. ...

..........

Sky & Telescope, SKY Online - Comet Hale-Bopp, Comet Hale-Bopp Is Coming!, By Edwin L. Aguirre, Adapted from Sky & Telescope, November 1995

Comet Hale-Bopp's Path

The following orbital elements (equinox 2000.0), calculated by Brian Marsden, are adapted from Minor Planet Circular 25,623:

Perihelion date T 1997 Mar. 31.96 UT
Perihelion distance q 0.9143 a.u.
Eccentricity e 0.9953
Argument of perihelion 130.57
Longitude of ascending node 282.47
Inclination i 89.43

........

NASA, Minor Planet Center Orbital Elements for Comet Hale-Bopp (1995-01), 22 February, 1996

Corrected Elements (J2000): Solution 22

Epoch: 2450520.50000 = 1997 Mar 13.00000
EC .995028866
QR .914124471
TP 2450539.66868 1997 Apr 1.16868
OM 282.47106
W 130.59479
IN 89.42762

The following (J2000) osculating orbital elements can be used to generate ephemeris data using two body programs. However, care must be taken to select an orbital element set with an epoch close to the desired ephemeris output times. ...

.......

Orbit and Ephemeris Information for Comet 1995 O1 Hale-Bopp, Don Yeomans - JPL, May 28, 1996

Additional observations through May 25, 1996, provided by the Minor Planet Center, have been used to update the orbit, ephemeris, and error analysis.

Object: Comet C/1995 O1 (Hale-Bopp)
Ref. Solution: 32
Planetary Ephemeris: DE403
No. Observations: 936
Observation Arc: 1993 Apr 27 - 1996 May 25

Residual Summary RA Dec Total

Mean .005 .003 .005
RMS, unweighted .667 .845 .761
Corrected Elements (J2000): Solution 32
Epoch 2450520.50000 = 1997 Mar 13.00000 Post-Fit Std.Dev.
e 0.995038361 .000005177
q 0.914119479 .000009551
Tp 2450539.6668732 .0031738483 1997 Apr 1.16687
Node 282.4709323 .0000289
w 130.5943673 .0003987
i 89.4283468 .0002580

ORBITAL ELEMENTS FOR COMET HALE-BOPP (1995 O1)

The following (J2000) osculating orbital elements can be used to generate ephemeris data using two body programs. However, care must be taken to select an orbital element set with an epoch close to the desired ephemeris output times.

Elements at other epochs:

Epoch (TDB)
  e q Node w i
Tp 1996 May 8.5
  .99643474 .916590274 282.471540 130.433689 89.409049
1997 Mar 31.946736
1996 Jun 01.0
  .99599928 .915777977 282.473417 130.484426 89.431978
1997 Apr 01.034170
1996 Jul 16.0
  .99550897 .914887986 282.473920 130.540972 89.436722
1997 Apr 01.116403
1996 Oct 04.0
  .99516562 .914311382 282.472611 130.579416 89.431303
1997 Apr 01.156988
1997 Mar 13.0
  .99503836 .914119479 282.470932 130.594367 89.428347
1997 Apr 01.166873
1997 Sep 09.0
  .99502984 .914060475 282.470095 130.590516 89.427269
1997 Apr 01.166023
e: Eccentricity
q: Perihelion passage distance (AU)
Node: Longitude of the ascending node (deg.)
w: Argument of perihelion (deg.)
i: Inclination (deg.)
Tp: Perihelion passage time (TDB)

Ephemeris data at 1 day and 5 day steps (O hours UTC) D.K. Yeomans (JPL) - May 28, 1996. Ephemeris computed using orbital solution No. 32 dated May 28, 1996. Magnitude predictions are only crude estimates.

Absolute (inertial) plane-of-sky ephemeris uncertainties (1-sigma) over this interval are as follows:

1996 Apr. - Sep. 03"
1997 Jan. - Feb. 10"
1997 Mar. 30"
1997 Apr. 20"

Ephemeris (with perturbations) for Comet C/1995 O1 (Hale-Bopp)

.........

NASA
From: DAN DUBRICK
Number: 587
Status: PUBLIC
To: ALL
Date/Time: 06-05-96 at 23:43
Subject: 5\28 Latest Comet Hale-Bo
Conference: 472...FN_SB-NASA_News

Latest Comet Hale-Bopp Ephemeris - May 28, 1996

The latest Comet Hale-Bopp Ephemeris is available for freqing from SpaceBase(tm) line 2 at (604)473-9358. File name to be requested is HBOP9606.TXT

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