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[jamsat-news:1542] ANS 196


AMSAT NEWS SERVICE
ANS 196

ANS is a free, weekly, news and information service of AMSAT North
America, the Radio Amateur Satellite Corporation. ANS reports on the
activities of a worldwide group of Amateur Radio operators who share an
active interest in designing, building, launching and communicating
through analog and digital Amateur Radio satellites.

ANS is first released via the AMSAT-NA 20-meter net held each Sunday
on 14.282 MHz. Pre-net operations start at 18:00 UTC, with current ANS
bulletins transmitted to the eastern U.S. at 19:00 UTC and to the western
U.S. at 19:30 UTC. ANS is also released worldwide via the AMSAT ANS
e-mail reflector.

AMSAT-NA is pleased to announce that recent (and future)
developments in Amateur Radio satellite technology will be discussed in
Atlanta, Georgia at the 19th Space Symposium and AMSAT-NA Annual
Meeting, October 5-6, 2001. The Symposium Chairman is Steve Diggs,
W4EPI. Contact W4EPI at:          w4epi@amsat.org

Information on AMSAT-NA is available at the following URL:

http://www.amsat.org <http://www.amsat.org/>  (or from)

AMSAT-NA
850 Sligo Avenue, Suite 600
Silver Spring, Maryland   20910-4703

Voice: 301-589-6062
FAX: 301-608-3410

Currently, AMSAT-NA supports the following (free) mailing lists:

* AMSAT News Service (ANS)
* General satellite discussion (AMSAT-BB)
* Orbit data (KEPS)
* Manned space missions (SAREX)
* District of Columbia area (AMSAT-DC)
* New England area (AMSAT-NE)
* AMSAT Educational Liaison mailing list (AMSAT-EDU)
* AMSAT K-12 Educational Liaison mailing list (AMSAT-K12)

A daily digest version is available for each list.

To subscribe, or for more list information, visit the following URL:

http://www.amsat.org/amsat/listserv/menu.html

In addition to regular membership, AMSAT-NA offers membership in the
President's Club. Members of the President's Club, as sustaining donors
To AMSAT Project Funds, will be eligible to receive additional benefits.
Initially, there will two levels for donations - Gold and Silver.
Application forms are available from the AMSAT-NA Office. For further
Information and details contact:

Daniel James, NN0DJ
AMSAT Vice President-Public Affairs
P.O. Box 297
Warroad, MN  56763-0297

NN0DJ can be reached at: (218) 386-1544  (or)  via e-mail at:
nn0dj@amsat.org

This edition of ANS is dedicated to the memory of Bennett Basore,
W5ZTN, of Stillwater, Oklahoma, who died in early July at age 78.
Basore served as ARRL Section Emergency Coordinator for some
30 years and most recently as Assistant Section Manager. He also
was net manager for the Oklahoma Phone Emergency Net, served
as an advisor to the Oklahoma State University Radio Cub, W5YJ,
and as a trustee for the Stillwater Amateur Radio Club repeater.
[ANS thanks the ARRL for this information]

ANS is always dedicated to the memory of past ANS editor 'BJ'
Arts, WT0N, and to the memory of long-time AMSAT supporter
Werner Haas, DJ5KQ.

ANS salutes Art Collins, 9CXX/W0CXX, who founded Collins Radio
Company. Collins set the standard for Amateur Radio equipment in the
1950s, 60s and 70s. W0CXX is among the inaugural group of 50
inductees into the CQ Amateur Radio Hall of Fame. The Hall was
established to recognize those individuals, whether licensed radio
amateurs or not, who significantly affected the course of Amateur Radio;
and radio amateurs, who, in the course of their professional lives, had a
significant impact on their professions or on world affairs. AMSAT and
OSCAR supporters/notables on the CQ Hall of Fame list include K1JT,
K1ZZ, W6SAI, W2SKE, W8JK, K7UGA, W6ZH, W3ASK, W1HR, KA9Q
and W3IWI. [ANS thanks CQ Amateur Radio magazine, published by CQ
Communications, Inc. for this information]

SB SAT @ AMSAT $ANS-196.01
AO-40 UPDATE

AMSAT NEWS SERVICE BULLETIN 196.01 FROM AMSAT HQ
SILVER SPRING, MD, JULY 15, 2001
TO ALL RADIO AMATEURS
BID: $ANS-196.01

AO-40 command station W4SM recently answered many questions
in an attempt to clear up any misconceptions concerning AO-40
operations in recent weeks - centered around the ATOS system and
the Arcjet cold firing. ANS has summarized this information:

* The old orbit was stable before any recent interaction, however,
perigee was very close (in some simulations as close as 160 km). There
was considerable drag at perigee, which continuously changed the mean
motion and probably contributed to the perturbation in ALON (the
mystery effect). Orbital tracking elements had to be frequently updated.
The rapidity of the perigee flyby also made magnetorquing very tricky.
To improve these things command stations attempted to raise the
perigee height with the decision to cold fire the Arcjet.

* The command software controlling the Arcjet was not faulty and there
is not any telemetry evidence to suggest any software error problems.

* The entire amount of ammonia aboard the satellite has been used and
it appears the TMFC (thermal mass flow controller) failed, passing far
more gas than it should have. As this was happening there was no
indication of this in the received telemetry. It is quite possible that there
was a slow leak in the ammonia tanks and if (in fact) there was a slow
leak - it is very fortunate we did not wait any longer to use the remaining
fuel. In addition, there is no evidence that the ammonia problem was due
to a command error.

* The Command Team is now looking at what is next for AO-40. The
momentum wheels have not yet been tested and the decision to deploy
(or not deploy) the solar panels is under investigation. The primary goal
remains to get AO-40 back into an orientation where the transponders
can be operational and RUDAK testing can be completed.

* AO-40 is in a stable orbit for much more than the next 20 years as
perigee is oscillating in a safe range between 810 and 1260 km.

* The Aux Battery is a nickel metal hydride (NiMH) battery. It
is currently off of trickle charge. These cells are quite happy fully
discharged and we believe that the battery will last longer if we do not
keep it on trickle charge (as we have no immediate need for it, we have
left it uncharged for now to prolong its life).

AO-40 is currently at approximately ALON/ALAT 311/5, accounting for
the much-improved telemetry signals on the first portion of the orbit. We
are torquing to approximately 320/0 (at which point the solar angle will be
close to 45 degrees) and the solar sensor may stop triggering, thereby
stopping the process.  If this does occur, it is a benign condition
because the Sun is moving away from us at almost 1 deg/day and very
quickly the solar angle will be re-established.

However, we will have to wait until the end of August to be able to move 
all the way back to 0/0. In the mean time, when we reach ~320/0 we will
stop magnetorquing and take pictures to verify our position.

Remember that there are still a number of items to check out. In
particular, we may have some days of limited or no transponder activity,
and even no beacon activity, while the RUDAK team uploads software
and checks out some of the RUDAK functions.

The AMSAT-DL web site is currently featuring an AO-40 status summary
format at:

http://www.amsat-dl.org/journal/adlj-p3d.htm

Stay tuned to ANS, the official source of AO-40 information.

[ANS thanks AMSAT-NA and AMSAT-DL for this information]

/EX

SB SAT @ AMSAT $ANS-196.02
AMSAT-UK COLLOQUIUM

AMSAT NEWS SERVICE BULLETIN 196.02 FROM AMSAT HQ
SILVER SPRING, MD, JULY 15, 2001
TO ALL RADIO AMATEURS
BID: $ANS-196.02

The 16th AMSAT-UK Colloquium will be held at Surrey University,
Guildford, Surrey, United Kingdom, July 27 - 29, 2001.

In addition to the standard program, additional attractions include a
satellite beginners session on Friday afternoon and tours of the Surrey
University satellite facilities. Microwave equipment testing, including
2.4GHz antenna gain testing, will be available. Also, the competition
for a new logo for the AMSAT OSCAR 40 satellite will take place at the
Colloquium, with winners to be announced.

Full details of the event are at:

http://www.uk.amsat.org/colloquium.htm

The provisional program is on the AMSAT-UK web site, check out:

http://www.uk.amsat.org/colloquium/program.htm

[ANS thanks Richard Limebear, G3RWL, for this information]

/EX

SB SAT @ AMSAT $ANS-196.03
STS-104 MISSION UNDERWAY

AMSAT NEWS SERVICE BULLETIN 196.03 FROM AMSAT HQ
SILVER SPRING, MD, JULY 15, 2001
TO ALL RADIO AMATEURS
BID: $ANS-196.03

The Space Shuttle Atlantis lifted off on time last week, and, after a
smooth climb to orbit, was quickly enroute to deliver a new doorway
to space to the International Space Station.

Atlantis Commander Steve Lindsey, Pilot Charlie Hobaugh and Mission
Specialists Janet Kavandi, Jim Reilly and Mike Gernhardt will install an
airlock named Quest on the station, increasing the orbiting complex's
onboard capabilities for maintenance and construction and completing a
major milestone in the station's orbital construction. The new airlock will
enable station crews to perform space walks in U.S. space suits without
the shuttle being present. This ability will enhance the station's
capabilities for maintenance and construction and complete a major
milestone in the station's orbital construction.

Commander Lindsey smoothly docked the space shuttle with the
International Space Station late Friday about 240 statute miles
above the northeastern coast of South America.  With both spacecraft
moving at about 17,500 mph, Lindsay moved Atlantis to the station at a
relative speed of about a tenth-of-a-foot per-second.

The five-member crew of Atlantis spent their fifth day in space
working with the Expedition-2 crew aboard the International Space
Station to continue the activation of the station's new airlock, including;

* testing nitrogen and oxygen lines that will be used during future shuttle
missions to replenish the airlock's tanks of high-pressure oxygen and
nitrogen;

* testing the airlock's space walk equipment;

* installing valves that will connect Quest to the station's environmental
control system.

In addition to checking and activating Quest's systems, the crews
removed the motor controllers from the airlock's berthing mechanism,
which are no longer needed now that the airlock is firmly attached to the
station.

After the airlock was attached to the station early Sunday morning, and
the first part of its checkout was completed, the shuttle and station crews
held a ribbon cutting for the new addition.

STS-104 Commander Lindsey and Pilot Charlie Hobaugh fired the
shuttle's engines for an hour Sunday night to boost the station to an
altitude of 238 by 235 statute miles (383 by 375 kilometers). Mission
Specialists Michael Gernhardt, Janet Kavandi and Jim Reilly also worked
on equipment and supply transfers between the shuttle and station.

The ARISS team reminds all that the ISS crews will be very busy during
the STS-104 mission (so voice operations may change tempo). In
addition, the Amateur Radio gear may need to be turned off for extended
periods for the safety of the ISS, shuttle, and their crews.

[ANS thanks NASA and ARISS for this information]

/EX

SB SAT @ AMSAT $ANS-196.04
ANS IN BRIEF

AMSAT NEWS SERVICE BULLETIN 196.04 FROM AMSAT HQ
SILVER SPRING, MD, JULY 15, 2001
TO ALL RADIO AMATEURS
BID: $ANS-196.04

ANS news in brief this week includes the following:

** As part of its escalated campaign to curb satellite signal piracy,
DirecTV, Inc. recently executed civil seizure and impoundment orders
against several businesses and individuals across the United States, and
seized several truckloads of equipment used to illegally reprogram
DirecTV access cards and steal DirecTV programming signals.
-SpaceDaily

** Several AMSAT-NA officers are working on a new AMSAT-NA Skills
Survey - intended to be distributed and collected primarily by e-mail and
printed form. The idea is to identify (new) potential volunteers. More
information as it becomes available. -ANS

**  Venus is key to understanding what the early Earth was like during
the early Proterozoic period when precious resources were formed.
While modern Venus is in a quiet state most of the time, is does enter
into short periods of intense volcanic activity where the old surface of
Venus is destroyed and a new one is created. In its early history when
life evolved, Earth worked in a similar way to modern Venus.
-SpaceDaily

** Patrick Clark, KC8BFD, a 17-year-old from Elkview, West
Virginia who is heavily involved in public service, emergency
Communications and youth recruitment of new radio amateurs, has been
named the 2001 Amateur Radio Newsline Young Ham of the Year. The
award is jointly sponsored by Newsline, Vertex Standard USA, Inc. and
CQ Magazine. Congratulations KC8BFD! -ANS, NewsLine

** The first Rocketdyne RS-68 flight engine has completed its flight
acceptance hot-fire test series at NASA's Stennis Space Center in
Mississippi. The engine was developed by the Rocketdyne Propulsion
and Power business of Boeing for the first-stage booster of the Boeing
Delta IV family of launch vehicles. -SpaceDaily

** Andy, W5ACM, reports that 73 Magazine will do another special
satellite issue in November. Andy would like to know if anyone would like
to participate! Material submission is easy, mostly e-mail. Contact Andy
for more information at: Andrew.MacAllister@daniel.com.
-Andy, W5ACM

--ANS BULLETIN END---

/EX

SB SAT @ AMSAT $ANS-196.05
WEEKLY SATELLITE REPORT PART 1

AMSAT NEWS SERVICE BULLETIN 196.05 FROM AMSAT HQ
SILVER SPRING, MD, JULY 15, 2001
TO ALL RADIO AMATEURS
BID: $ANS-196.05

Phase 3D / AMSAT OSCAR 40 / AO-40
Launched: November 16, 2000 aboard an Ariane 5 launcher
from Kourou, French Guiana. Status: S-Band transmitter is active.
The RUDAK system has been activated.

AO-40 experimental transponder operation started on May 05, 2001 at
approximately 08:00 UTC when the U-band and L1-band uplinks were
connected to the S-2 transmitter passband downlink via the Matrix
switch. Transponder operation is currently suspended.

G6LVB has described how to use an offset-dish for S-downlink at:
www.g6lvb.com/60cm.htm

Three programs to convert RUDAK WOD (whole orbit data) are available
at: www.amsat.org/amsat/ftpdelta.html

[ANS thanks AMSAT-NA, AMSAT-DL and the ARRL for this information]

INTERNATIONAL SPACE STATION/ARISS
Worldwide packet uplink:            145.990 MHz
Region 1 voice uplink:                 145.200 MHz
Region 2/3 voice uplink:              144.490 MHz
Worldwide downlink:                    145.800 MHz
TNC callsign                                 NOCALL

ARISS initial station launched September 2000 aboard shuttle Atlantis.
ARISS is made up of delegates from major national Amateur Radio
organizations, including AMSAT.

Status: Operational. Voice contacts with ISS have been made recently.
The ISS packet station is available for UI packets (APRS or UI QSL).
The mailbox and keyboard are currently disabled. Please see the packet
section of the ARISS web page before attempting to first work ISS on
packet.

The ISS daily crew schedule (which gives an idea when crew members
have free time and may be available for Amateur Radio operations) can
be found at:

http://spaceflight.nasa.gov/station/timelines/2001/may/index.html

U.S. callsign:                  NA1SS
Russian callsigns:          RS0ISS, RZ3DZR

The QSL routes for W/VE stations working NA1SS aboard the International Space Station:

U.S. stations:              	Margie Bourgoin KB1DCO
                                    	Attn: ARISS Expedition-1 (or 2) QSL
                                    	ARRL, 225 Main Street
                                    	Newington, Connecticut 06111

Canadian stations:      	Radio Amateurs of Canada
                                    	Attn: ARISS Expedition-1 (or 2) QSL
                                    	720 Belfast Road, Suite 217
                                    	Ottawa, Ontario K1G 0Z5

European stations:	AMSAT-France
16, rue de la Vallee
91360 Epinay sur Orge, France

A self-addressed, stamped envelope is required to get a QSL in return.
The ARISS international group has not yet finalized a QSL card design.
It will be a few months before cards become available. More information
about the project can be found on the ARISS web site at:

http://ariss.gsfc.nasa.gov

[ANS thanks ARISS team member Will Marchant, KC6ROL, for this
information]

RADIO SPORT RS-12
Uplink                           145.910 to 145.950 MHz CW/SSB
Downlink                       29.410 to 29.450 MHz CW/SSB
Beacon                         29.408 MHz
Launched: February 5, 1991 aboard a Russian Cosmos C launcher
Status: RS-12 was re-activated in mode-A on January 1, 2001

Jerry, K5OE, reports working several stations on RS-12 recently on
mode-A and did not hear any signal distortion from the satellite downlink.

The latest information on RS-12 and RS-13 can be found on the AC5DK
RS-12/13 Satellite Operators page at:

http://www.qsl.net/ac5dk/rs1213/rs1213.html

[ANS thanks Kevin Manzer, AC5DK, for RS-12 information]

RADIO SPORT RS-15
Uplink                           145.858 to 145.898 MHz CW/SSB
Downlink                       29.354 to 29.394 MHz CW/SSB
Beacon                         29.352 MHz (intermittent)
SSB meeting frequency     29.380 MHz (unofficial)
Launched: December 26, 1994 from the Baikonur Cosmodrome
Status: Semi-operational, mode-A, using a 2-meter uplink and a
10-meter downlink

Dave, WB6LLO, has operating information for both RS-15 on his
Web site. In addition to satellite data, antenna information for
mode-A operation is also featured. The WB6LLO web site URL is:

http://home.san.rr.com/doguimont/uploads

[ANS thanks Dave Guimont, WB6LLO, for this information]

OSCAR 10 AO-10
Uplink               435.030 to 435.180 MHz CW/LSB
Downlink           145.975 to 145.825 MHz CW/USB
Beacon             145.810 MHz (unmodulated carrier)
Launched: June 16, 1983 by an Ariane launcher from Kourou,
French Guiana. Status: Semi-operational, mode-B. AO-10 has
been locked into a 70-cm uplink and a 2-meter downlink for several
years.

DX continues to be heard and worked on AO-10.

W4SM has more information about the satellite at the following URL:

http://www.cstone.net/~w4sm/AO-10.html

[ANS thanks Stacey Mills, W4SM, for his AO-10 status information
and web site]

AMRAD AO-27
Uplink               145.850 MHz FM
Downlink           436.795 MHz FM
Launched: September 26, 1993 by an Ariane launcher from Kourou,
French Guiana. Status: Operational, mode J.

Periodically, AO-27's analog repeater will be turned off for a few days at
a time to enable ground controllers to gather Whole Orbital Data (WOD),
to verify the health of the satellite.

An AO-27 question-and-answer page is available on the AMSAT-NA web
site. The URL is: http://www.amsat.org/amsat/intro/ao27faq.html

AO-27 uses a method called Timed Eclipse Power Regulation (TEPR) to
regulate the on-board batteries. In simple terms, TEPR times how long
the satellite has been in an eclipse (or in the sun) and decides what
subsystems to turn on or off. The AO-27 pages on the AMSAT-NA web
site include an explanation of TEPR AO-27 operations (at):

http://www.amsat.org/amsat/sats/n7hpr/ao27.html

TEPR states on AO-27 were reset on March 24, 2001 as follows:

TEPR 4 is 38 / TEPR 5 is 78 (TEPR 5 is now 20 minutes long)

[ANS thanks AMRAD for AO-27 information]

UO-14
Uplink               145.975 MHz FM
Downlink           435.070 MHz FM
Launched: January 22, 1990 by an Ariane launcher from Kourou,
French Guiana. Status: Operational, mode J

Tim, KG8OC, features UO-14 information on the Michigan AMSAT
web site -- point your web browser to the following URL:

http://www.qsl.net/kg8oc

[ANS thanks Chris Jackson, G7UPN/ZL2TPO, for UO-14 information]

JAS-1b FO-20
Uplink               145.90 to 146.00 MHz CW/LSB
Downlink           435.80 to 435.90 MHz CW/USB
Launched: February 07, 1990 by an H1 launcher from the Tanegashima
Space Center in Japan. Status: Operational. FO-20 is in mode JA
continuously

Tak, JA2PKI, reported FO-20 control station operators believe that the
UVC (Under Voltage Controller) now is regulating the transponder. The
controller monitors battery voltage and tries to protect the batteries from
over discharge.

[ANS thanks Kazu Sakamoto, JJ1WTK, for the FO-20 status reports]

JAS-2 FO-29
Launched: August 17, 1996, by an H-2 launcher from the Tanegashima
Space Center in Japan. Status: Operational

Voice/CW Mode JA
Uplink               145.90 to 146.00 MHz CW/LSB
Downlink           435.80 to 435.90 MHz CW/USB

Digital Mode JD
Uplink               145.850 145.870 145.910 MHz FM
Downlink           435.910 MHz 1200-baud BPSK or 9600-baud FSK
Callsign             8J1JCS
Digitalker           435.910 MHz

Last reported, the JARL FO-29 command station announced the
operation schedule of FO-29 through October 2001 - is mode JA

Mineo, JE9PEL, has a FO-29 satellite telemetry analysis program that
will automatically analyze all digital telemetry from the satellite (such as
current, voltage and temperature). The JE9PEL FO-29/shareware is
available at the following URL:

http://www.ne.jp/asahi/hamradio/je9pel/

[ANS thanks Kazu Sakamoto, JJ1WTK, for the FO-29 status reports]

/EX

SB SAT @ AMSAT $ANS-196.06
WEEKLY SATELLITE REPORT PART 2

AMSAT NEWS SERVICE BULLETIN 196.06 FROM AMSAT HQ
SILVER SPRING, MD, JULY 15, 2001
TO ALL RADIO AMATEURS
BID: $ANS-196.06

TIUNGSAT-1
Uplink               145.850 or 145.925 MHz 9600-baud FSK
Downlink           437.325 MHz
Broadcast callsign  	MYSAT3-11
BBS                        	MYSAT3-12

Launched: September 26, 2000 aboard a converted Soviet ballistic
missile from the Baikonur Cosmodrome. Status: Operational at
38k4-baud FSK

Chris, G7UPN, tells ANS that TiungSat-1 has been operating at a data
rate of 38k4. Data recovery at 38k4 is reported to be extremely good with
efficiencies near 100%. The output power is at 8-watts "which should
provide a very good downlink," said Chris, adding "the downside is that
with the high power transmitter operating, the power budget is negative
so we can't support continuous operation."

According to G7UPN, TiungSat-1 now requires the Amateur Radio
station to switch the downlink 'on' when the satellite comes into range.
The way this works is for the ground station software to send a request
to the spacecraft to switch the downlink on. The spacecraft receives this
request and checks the battery voltage to see if it can support the
operation, and if it can it will activate the downlink.

TiungSat-1 is Malaysia's first micro-satellite and in addition to
commercial land and weather imaging payloads offers FM and FSK
Amateur Radio communication.

TiungSat-1, named after the mynah bird of Malaysia, was developed as
a collaborative effort between the Malaysian government and Surrey
Satellite Technology Ltd.

For more information on TiungSat-1, visit the following URL:

http://www.yellowpages.com.my/tiungsat/tiung_main.htm

[ANS thanks Chris Jackson, G7UPN/ZL2TPO, for this information]

KITSAT KO-25
Uplink               145.980 MHz FM (9600-baud FSK)
Downlink           436.500 MHz FM
Broadcast Callsign         HL02-11
BBS                             HL02-12

Launched: September 26, 1993 by an Ariane launcher from Kourou,
French Guiana. Status: Operational

Jim, AA7KC, reports KO-25 returned to service on July 12th. Downlink
efficiency is in the 50% range. Traffic is moderate to heavy. The KO-25
command team had reported the on-board computer (OBC) of KO-25
crashed on June 19, 2001. The team was successful in uploading new
software under the direction of HL0ENJ.

[ANS thanks Jim Weisenberger, AA7KC, for this information]

UOSAT UO-22
Uplink               145.900 or 145.975 MHz FM 9600-baud FSK
Downlink           435.120 MHz FM
Broadcast Callsign        UOSAT5-11
BBS                             	UOSAT5-12

Launched: July 17, 1991 by an Ariane launcher from Kourou,
French Guiana. Status: Operational

Jim, AA7KC, reports UO-22 is operational with good downlink efficiency
and heavy traffic, both individual and SatGate. Many international
gateways are represented on the satellite.

More information on the satellite is available at the following URL:

http://www.sstl.co.uk/

[ANS thanks Chris Jackson, G7UPN/ZL2TPO, for UO-22 information and
Jim Weisenberger, AA7KC, for status information]

OSCAR-11
Downlink              145.825 MHz FM (1200-baud AFSK)
Mode-S Beacon    2401.500 MHz
Launched: March 1, 1984 by a Delta-Thor rocket from Vandenberg Air
Force Base in California. Status: Operational

Clive, G3CWV, reported to ANS that it has been an uneventful time for
OSCAR-11 during the period of May 15-June 9, 2001. 

Battery voltage observed during daylight passes has continued to
decrease. The average value observed was 13.3 volts with a range of
13.1 to 13.5 volts. The internal temperatures have continued to
decrease, now -0.2 and -1.6 Celsius for battery and telemetry electronics
respectively.

The magnetometer calibrations have steadily changed during the many
years in orbit. Although the changes are small and are not noticeable on
a plot of individual channels, they do have a considerable effect when
the total magnetic field is calculated. The spin period has also varied,
now between 300 and 344 seconds, with the attitude control working
normally.

The mode-S beacon is active, transmitting an unmodulated carrier. This
beacon is a useful test source for those testing mode-S converters for
AO-40.

Users of OSCAR-11 should note that the hardware generated time in the
ASCII telemetry is now 15.5 minutes ahead of UTC, and the date is three
days advanced. Unfortunately these errors cannot be corrected.

The operating schedule is as follows:

ASCII status (210 seconds)
ASCII bulletin (60 seconds)
BINARY SEU (30 seconds)
ASCII TLM (90 seconds)
ASCII WOD (120 seconds)
ASCII bulletin (60 seconds)
BINARY ENG (30 seconds)
 
The ASCII bulletin is currently a static message, detailing modes and
frequencies of all active amateur radio satellites.

More information on OSCAR-11 is available at the following URL:

http://www.users.zetnet.co.uk/clivew/

[ANS thanks Clive Wallis, G3CWV, for OSCAR-11 status information]

PACSAT AO-16
Uplink                           145.90 145.92 145.94 145.96 MHz FM
                                     (using 1200-baud Manchester FSK)
Downlink                       437.025 MHz SSB (RC-BPSK 1200-baud PSK)
Mode-S Beacon            2401.1428 MHz
Broadcast Callsign:       PACSAT-11
BBS                               PACSAT-12

Launched: January 22, 1990 by an Ariane launcher from Kourou,
French Guiana. Status: Semi-operational, the digipeater command is on.

Telemetry is as follows:

uptime is 516/18:31:47.  Time is Fri Jul 13 22:08:51 2001
+X (RX) Temp   -12.104 D  RX Temp          0.603 D
Bat 1 V          1.225 V  Bat 2 V          1.117 V
Bat 3 V          1.145 V  Bat 4 V          1.208 V
Bat 5 V          1.110 V  Bat 6 V          1.199 V
Bat 7 V          1.117 V  Bat 8 V          1.169 V
Bat 1 Temp       1.814 D  Bat 2 Temp       1.814 D
Baseplt Temp     1.814 D  PSK TX RF Out    0.698 W
RC PSK BP Temp  -6.658 D  RC PSK HPA Tmp  -6.658 D
+Y Array Temp  -22.995 D  PSK TX HPA Tmp  -3.027 D
+Z Array Temp  -16.339 D
Total Array C= 0.038 Bat Ch Cur=-0.100 Ifb= 0.049 I+10V= 0.072
TX:1006 BCR:7A PWRC:36D BT:1E WC:25 EDAC:F3

A new WOD collection of current graphics along with general
Information and telemetry samples can be found at:

www.telecable.es/personales/ea1bcu

[ANS thanks Miguel Menendez, EA1BCU, for AO-16 status information]

UoSAT-12 UO-36
Uplink               145.960 MHz (9600-baud FSK)
Downlink           437.025 MHz 437.400 MHz
Broadcast Callsign         UO121-11
BBS                                UO121-12

Launched: April 21, 1999 by a Russian launcher from the Baikonur
Cosmodrome. Status: Operational

 UO-36 carries a number of imaging payloads, digital store-and-forward
communications and mode L/S transponders. 

NASA has demonstrated on UO-36 the ability to use standard Internet
protocols to communicate with an orbiting spacecraft (just like any node
on the Internet). NASA has been developing this project by working with
the commercial payload aboard UoSAT-12.

The BBS is open, although uploading and downloading may be disabled
at times.

The VK5HI viewer shareware for UO-36 is available on the AMSAT-NA
web site at the following URL:

ftp://ftp.amsat.org/amsat/software/win32/display/ccddsp97-119.zip

Further information on UO-36 is available from: http://www.sstl.co.uk/

[ANS thanks Chris G7UPN/ZL2TPO, and the University of Surrey for this
information]

ITAMSAT IO-26
Uplink               145.875 145.900 145.925 145.950 MHz FM (1200-baud)
Downlink           435.822 MHz SSB
Broadcast Callsign         ITMSAT-11
BBS                                ITMSAT-12

Launched: September 26, 1993 by an Ariane launcher from Kourou,
French Guiana. Status: Semi-operational, the digipeater function is on
and open for APRS users.

[ANS thanks ITAMSAT Project Manager Alberto E. Zagni, I2KBD, for
IO-26 information]

/EX

SB SAT @ AMSAT $ANS-196.07
WEEKLY SATELLITE REPORT PART 3

AMSAT NEWS SERVICE BULLETIN 197.06 FROM AMSAT HQ
SILVER SPRING, MD, JULY 15, 2001
TO ALL RADIO AMATEURS
BID: $ANS-196.07

THE FOLLOWING ARE IN ORBIT BUT ARE NON-OPERATIONAL
AT THIS TIME:

TMSAT-1 TO-31
Uplink               145.925 MHz (9600-baud FSK)
Downlink           436.925 MHz (9600-baud FSK)
Broadcast Callsign:        TMSAT1-11
BBS                                TMSAT1-12 

Launched: July 10, 1998 by a Zenit rocket from the Baikonur
Cosmodrome. Status: Non-operational, no data downlinked
since December 18, 2000.

Chris G7UPN, (UoSAT operations manager) reports the
following to ANS:

The TO-31 downlink will be off over most areas, with the exception of
Europe and Thailand. This is required to allow control stations to
recondition the battery with minimum power drain.

ProcMail V2.00G has been released by G7UPN. This software permits
the processing of image files from TO-31. It has been posted to the
AMSAT-NA FTP site at the following URL:

http://www.amsat.org/amsat/software/win32/wisp

Many of the high-resolution color images transmitted by TMSAT are
Compressed using a UoSAT compression format. This format is
supported by the VK5HI CCD display program.

[ANS thanks Chris Jackson, G7UPN/ZL2TPO, for TO-31 status
information]

LUSAT LO-19
Uplink                           145.84 145.86 145.88 145.90 MHz FM
                                     (using 1200-baud Manchester FSK)
CW downlink                 437.125 MHz
Digital downlink             437.150 MHz SSB (RC-BPSK 1200-baud PSK)
Broadcast Callsign         LUSAT-11
BBS                                LUSAT-12
Launched: January 22, 1990 by an Ariane launcher from Kourou, French
Guiana. Status: Beacon only. The CW beacon is sending eight telemetry
channels and one status channel on 437.126 MHz. No BBS service is
available. The digipeater is not active.

Telemetry is as follows:

Time is Fri Jul 13 21:53:51 2001
CW-Code: avt aba av6 abn au6 a6v ttu aee
 5V-reg.:   4.89 V      8.5V-reg:   8.68 V
 10V-Bat:  10.94 V      10V-Curr:  114.1 mA
 TX-Pwr :  0.899 W      TX-Temp.:  -0.46 ?C
 +Z-Sol.:   0.30 V      Box-Temp:   3.56 ?C

CW-Code: avt aba av6 abn aub a6u ttu aee
 5V-reg.:   4.89 V      8.5V-reg:   8.68 V
 10V-Bat:  10.94 V      10V-Curr:  113.4 mA
 TX-Pwr :  0.899 W      TX-Temp.:  -0.46 ?C
 +Z-Sol.:   0.30 V      Box-Temp:   3.20 ?C

General information and decode values of
CW telemetry can find it in:
www.telecable.es/personales/ea1bcu/lo19

Mineo, JE9PEL, has recorded LO-19 CW and PSK telemetry and placed
the information on his Internet homepage site at:

http://www.ne.jp/asahi/hamradio/je9pel/

General information and telemetry samples can be found at:

www.telecable.es/personales/ea1bcu

[ANS thanks Miguel Menendez, EA1BCU, for LO-19 status information]

SO-41  SAUDISAT-1A

Uplink               to be released
Downlink           437.075 MHz 
Broadcast Callsign         SASAT1-11
BBS                                SASAT1-12

Launched: September 26, 2000 aboard a converted Soviet ballistic
missile from the Baikonur Cosmodrome. Status: Unknown, this satellite
has been in orbit for almost 8 months. ANS has received no additional
information.

When/if operational, SaudiSat-1A will operate as 9600-baud digital
store-and-forward systems as well analog FM repeater mode capability.
One of two new ham satellites from the Kingdom of Saudi Arabia built by
the Space Research Institute at the King Abdulaziz City for Science and
Technology.

SO-42  SAUDISAT-1B
Uplink               to be released
Downlink           436.775 MHz
Broadcast Callsign         SASAT2-11
BBS                                SASAT2-12
Launched: September 26, 2000 aboard a converted Soviet ballistic
missile from the Baikonur Cosmodrome. Status: Unknown, this satellite
has been in orbit for almost 8 months. ANS has received no additional
information.

When/if operational, SaudiSat-1B will operate as 9600-baud digital
store-and-forward systems as well analog FM repeater mode capability.
One of two new ham satellites from the Kingdom of Saudi Arabia built by
the Space Research Institute at the King Abdulaziz City for Science and
Technology.

SUNSAT SO-35
Mode J Uplink:               145.825 MHz FM
Mode J Downlink:           436.250 MHz FM

Mode B Uplink:               436.291 MHz FM
Mode B Downlink:          145.825 MHz FM

Launched: February 23, 1999 by a Delta II rocket from Vandenberg Air
Force Base in California. Status: Non-operational

The SunSat team released the following statement, dated
February 1, 2001:

We regret to announce that the last communication with SunSat from our
ground station at the Electronic Systems Laboratory at Stellenbosch
University took place recently. We are certain, after having performed
several tests since the last contact, that an irreversible, physical failure
has occurred on the satellite. It is therefore unlikely that we will have
any further contact with SunSat, apart from the occasional visual sighting
by telescope!

When it was operational the SunSat package included 1200 and 9600
baud digital store-and-forward capability and a voice 'parrot' repeater
system in addition to Mode B/J operation with two VHF and two UHF
transmit-receive systems.

For more information on SunSat visit the following URL:

http://sunsat.ee.sun.ac.za 

[ANS thanks Garth Milne, ZR1AFH, for this information]

RADIO SPORT RS-13
Uplink                           21.260 to 21.300 MHz CW/SSB
Downlink                       145.860 to 145.900 MHz CW/SSB
Beacon                         145.860 MHz

Launched: February 5, 1991 aboard a Russian Cosmos C launcher
Status: non-operational (last operational in mode-T)

RS-12 was re-activated in January 2001. Prior to this switch RS-13 was
operational (mode T), but was apparently turned off following the recent
RS-12 switch.

The latest information on RS-12 and RS-13 can be found on the AC5DK
RS-12/13 Satellite Operators page at:

http://www.qsl.net/ac5dk/rs1213/rs1213.html

[ANS thanks Kevin Manzer, AC5DK, for this information]

KITSAT KO-23
Uplink               145.900 MHz FM (9600-baud FSK)
Downlink           435.170 MHz FM
Broadcast Callsign         HLO1-11
BBS                                HLO1-12
Launched: August 10, 1992 by an Ariane launcher from Kourou,
French Guiana. Status: Intermittent operation with the downlink
transmitter operating at unpredictable intervals.

Jim, AA7KC, reported that KO-23's downlink transmitter continues in
non-operational status. Jim says that KO-23 shows some signs of trying
to recover, but no useful data has been downlinked. The duration of this
status is unpredictable. No data has been received since
October 28, 2000.

KyungHee Kim, HL0ENJ, reports (from the KO-23 control team) that part
of the problem with non-operation has been the power budget aboard the
satellite. "We are not sure when the bird might turn off again due to
insufficient power. The capability of the onboard power system has been
less and less," said Kim. HL0ENJ also noted that as of October 30, 2000
the onboard computer was reset and a reboot of operational software
is/was underway.

[ANS thanks Jim Weisenberger, AA7KC, and KyungHee Kim, HL0ENJ,
for KO-23 status information]

TECHSAT-1B GO-32
Downlink           435.225 MHz using HDLC telemetry
Launched: July 10, 1998 by a Russian Zenit rocket from the Baikonur
Cosmodrome. Status: Semi-operational.

Efforts were reported to be underway to bring GO-32 on line, however,
no information has been received by ANS (the last report was dated
November 1999).

Last reported, the satellite does transmit a 9600-baud burst every 30
seconds (the GO-32 beacon sends one short telemetry status
transmission of 44 bytes) and upon request the complete telemetry
buffer.

[ANS has no further information]

PANSAT PO-34
Uplink/downlink frequency (listed on the PanSat web site) 436.500 MHz
Launched: October 30, 1998 by the Shuttle Discovery. Status: Unknown

The satellite is not available for general uplink transmissions.

The Naval Postgraduate School developed PanSat. At the time of
launch, PanSat spread-spectrum digital transponders were promised to
be available to Amateur Radio operators along with software to utilize
this technology. To date, this has not happened.

For more information, visit the official PanSat web site at:

http://www.sp.nps.navy.mil/pansat/

PanSat was the featured cover article on the July/August 1999 issue of
the AMSAT-NA Journal (the story written by KD6DRA and N7HPR).

[ANS has no further information]

DOVE DO-17
Downlink           145.825 MHz FM (1200-baud AFSK)
                          2401.220 MHz
Launched: January 22, 1990 by an Ariane launcher from Kourou,
French Guiana. Status: Non-operational.

DOVE stopped transmitting in March 1998. The 145.825 MHz and
2401.220 MHz downlinks are off the air and the satellite has not
responded to ground station control.

[ANS has no further information]

WEBERSAT WO-18
Downlink           437.104 MHz SSB (1200 baud PSK AX.25)
Launched: January 22, 1990 by an Ariane launcher from Kourou,
French Guiana. Status: Non-operational.

WO-18 was last reported to be in MBL mode after a software crash.

[ANS has no further information]

SEDSAT-1 SO-33
Downlink           437.910 MHz FM (9600-baud FSK)
Launched: October 24, 1998 by a Delta 2 rocket from Cape Canaveral,
Florida. Status: Semi-operational.

The satellite is not currently available for uplink transmissions and the
image and transponder recovery efforts have been unsuccessful.

SedSat-1 signifies Students for the Exploration and Development of
Space (satellite number one).

SedSat-1 has downlinked months worth of telemetry data on the
performance of its electrical power system parameters. The Nickel
Metal Hydride batteries on the spacecraft were experimental and
experienced some abuse due to a power negative situation. This
information has provided NASA with useful information. With the
exception of the imaging system and the use of the transponders,
SedSat-1 has been judged a success.

For more information on SedSat-1 visit the satellite web site at the
following URL:

http://seds.uah.edu/projects/sedsat/sedsat.htm

[ANS has no further information]

/EX

--ANS END---

ANS would like to thank Mike Seguin, N1JEZ, ANS principal satellite
investigator, for helping provide current satellite information.

Please send any amateur satellite news or reports to:

ans-editor@amsat.org

Daniel (Dan) James
AMSAT News Service Bulletin Editor
AMSAT-NA Vice President/Public Affairs
Amateur callsign: NN0DJ
Grid Square EN28iv
Warroad, Minnesota U.S.A.
E-mail: nn0dj@amsat.org

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