Date: Sat, 25 Jul 92 11:42:11 From: Space Digest maintainer Reply-To: Space-request@isu.isunet.edu Subject: Space Digest V15 #037 To: Space Digest Readers Precedence: bulk Space Digest Sat, 25 Jul 92 Volume 15 : Issue 037 Today's Topics: Antimatter (was propulsion questions) Astronaut Information Astronomy Lab for MS Windows 3.X - BETA TESTERS NEEDED FYI No. 97: NASA Issues Space Station Strategic Plan... Galileo Antenna. What's left to try? (4 msgs) Galileo Update - 07/24/92 SPIF Update TSS-1 launch time Two-Line Orbital Element Sets, Part 1 Wanted satellite tracking program for GPS sats Welcome to the Space Digest!! Please send your messages to "space@isu.isunet.edu", and (un)subscription requests of the form "Subscribe Space " to one of these addresses: listserv@uga (BITNET), rice::boyle (SPAN/NSInet), utadnx::utspan::rice::boyle (THENET), or space-REQUEST@isu.isunet.edu (Internet). ---------------------------------------------------------------------- Date: Sat, 25 Jul 1992 00:06:59 GMT From: Mike Wexler Subject: Antimatter (was propulsion questions) Newsgroups: sci.space jdnicoll@watyew.uwaterloo.ca (James Davis Nicoll) writes: > Given that one can mix the antimatter-reaction mass ratio to get >the Vexhaust one wants, the dangers of standing in the vicinity of the >exhaust of an antimatter powered ship could be *identical* to that of >standing inthe vicinity of a conventional ship. Actually there is one piece of information missing here. In a conventional rocket most of the exhaust is being used to push more fuel closer to orbit. In an antimatter rocket, you have a much higher payload/fuel ratio, so for the same payload, there will be much less exhaust. -- Mike Wexler (mikew@kpc.com) ------------------------------ Date: 24 Jul 92 18:17:00 GMT From: ganesh@drystone.attmail.com Subject: Astronaut Information Can anybody provide me some information about where and how to apply for being an astronaut. I would be greatful if you could provide any information about requirements etc. Thanks in advance. Ganesh (ganesh@drystone.attmail.com) -------------------------------------------------------------------- ------------------------------ Date: 24 Jul 92 21:35:04 GMT From: Mike Newberry Subject: Astronomy Lab for MS Windows 3.X - BETA TESTERS NEEDED Newsgroups: comp.windows.ms,comp.ibm.pc.misc,sci.astro,sci.space,sci.edu,comp.windows.ms.programmer,comp.binaries.ibm.pc.d In article <1992Jul23.003615.13232@access.digex.com> mheney@access.digex.com (Michael K. Heney) writes: >My mail also got bounced. Send me a message and I'll pass along the >information you were asking for - I won't clutter the newsgroup any more >than I must. Thanks. The mail I tried to send you last week with name, address, computing hardware, etc. ALSO BOUNCED. send me email. Mike Newberry newberry@as,.arizona.edu ------------------------------ Date: Sat, 25 Jul 1992 00:14:06 GMT From: keith@msmri.med.ubc.ca Subject: FYI No. 97: NASA Issues Space Station Strategic Plan... Newsgroups: sci.research,sci.space In article <1992Jul24.185457.18611@relay.nswc.navy.mil> rsherme@nswc-wo.navy.mil (Russel Shermer) writes: >Posted for: >Public Information Division >American Institute of Physics >Contact: Richard M. Jones >(202) 332-9661 >Send email inquiries to fyi@aip.org > > >NASA Issues Space Station Strategic Plan; Station Opponents >Announce Plans > >FYI No. 97, July 24, 1992 > >In a new 48-page report, NASA has presented its vision of Space >Station Freedom's projected accomplishments, mission, goals, and >objectives. As might be expected, this report provides an >optimistic and persuasive case for the station, and will no doubt >be cited by proponents of the program in upcoming House and Senate >debates over the future of the station. Some of the reports >highlights: Is anyone planning on scanning this report into GIF files and making it available via anonyomous ftp? (If the files are not too big). This has been done previously with shuttle documents. Keith S. Cover Dept. of Physics University of British Columbia Vancouver, B.C., Canada keith@msmri.med.ubc.ca ------------------------------ Date: Sat, 25 Jul 1992 02:58:08 GMT From: Ron Baalke Subject: Galileo Antenna. What's left to try? Newsgroups: sci.space In article <1992Jul21.190805.4575@ucsu.Colorado.EDU>, knapp@spot.Colorado.EDU (David Knapp) writes... > >Perhaps I've missed some crucial posts (which is entrirely possible given >a quirky news server) but I haven't seen a lot of news regarding the >details of the Galileo Antenna. > >What can be attempted? Thruster bursts? Fast rotation? After the Earth flyby when the thermal conditions are more favorable, the deployment motors will be pulsed to hammer the ballscrew which drives the shaft which opens the antenna. An additonal 1.5 revolution turn of the ballscrew is expected. >What is the confidence that *some* technique will succeed? The best news occurred in the past week when the motors were turned on twice for a two second duration each time. The data indicates ballscrew had turned and this provides a lot of confidence in the upcoming pulsing attempt. ___ _____ ___ /_ /| /____/ \ /_ /| Ron Baalke | baalke@kelvin.jpl.nasa.gov | | | | __ \ /| | | | Jet Propulsion Lab | ___| | | | |__) |/ | | |__ M/S 525-3684 Telos | Most of the things you /___| | | | ___/ | |/__ /| Pasadena, CA 91109 | worry about will never |_____|/ |_|/ |_____|/ | happen. ------------------------------ Date: Fri, 24 Jul 1992 20:31:49 GMT From: "David W. Levine" Subject: Galileo Antenna. What's left to try? Newsgroups: sci.space What's the time frame for the "Pulse Hammering?" I know it's after the second Earth flyby, but how soon after? David W. Levine -- IBM Thomas J. Watson Research Center dwl@watson.ibm.com -- (914) 784-7427 My Opinions, IBM's hardware. -- ------------------------------ Date: Sat, 25 Jul 1992 05:24:10 GMT From: Ron Baalke Subject: Galileo Antenna. What's left to try? Newsgroups: sci.space In article <1992Jul24.203149.20786@watson.ibm.com>, dwl@watson.ibm.com (David W. Levine) writes... >What's the time frame for the "Pulse Hammering?" I know it's after >the second Earth flyby, but how soon after? The exact day hasn't been determined yet, but it will be in either December or January. The Earth flyby in on December 8. ___ _____ ___ /_ /| /____/ \ /_ /| Ron Baalke | baalke@kelvin.jpl.nasa.gov | | | | __ \ /| | | | Jet Propulsion Lab | ___| | | | |__) |/ | | |__ M/S 525-3684 Telos | Most of the things you /___| | | | ___/ | |/__ /| Pasadena, CA 91109 | worry about will never |_____|/ |_|/ |_____|/ | happen. ------------------------------ Date: 24 Jul 1992 14:37:19 -0700 From: Steven Robiner Subject: Galileo Antenna. What's left to try? Newsgroups: sci.space In article <1992Jul24.191039.11492@elroy.jpl.nasa.gov> baalke@kelvin.jpl.nasa.gov writes: >The best news occurred in the past week when the motors were >turned on twice for a two second duration each time. The data indicates >ballscrew had turned and this provides a lot of confidence in the >upcoming pulsing attempt. If that doesn't work.... Has anyone considered the possibility of spinning the probe very fast along the axis of the antenna? Perhaps the centriptal force might pull the antenna into place. =steve= >>What is the confidence that *some* technique will succeed? > >The best news occurred in the past week when the motors were >turned on twice for a two second duration each time. The data indicates >ballscrew had turned and this provides a lot of confidence in the >upcoming pulsing attempt. > ___ _____ ___ > /_ /| /____/ \ /_ /| Ron Baalke | baalke@kelvin.jpl.nasa.gov > | | | | __ \ /| | | | Jet Propulsion Lab | > ___| | | | |__) |/ | | |__ M/S 525-3684 Telos | Most of the things you >/___| | | | ___/ | |/__ /| Pasadena, CA 91109 | worry about will never >|_____|/ |_|/ |_____|/ | happen. > ------------------------------ Date: Sat, 25 Jul 1992 02:45:07 GMT From: Ron Baalke Subject: Galileo Update - 07/24/92 Newsgroups: sci.space,sci.astro Forwarded from Neal Ausman, Galileo Mission Director GALILEO MISSION DIRECTOR STATUS REPORT POST-LAUNCH July 17 - 23, 1992 SPACECRAFT 1. On July 17, realtime commands were sent to verify the commandability of the spacecraft following the Command Processor Assembly (CPA) configuration problem on Wednesday, July 15. A single frame command followed by a multi-frame command were sent and successfully received by the spacecraft. 2. On July 19, real-time commands, previously attempted on July 15 and unsuccessfully received by the spacecraft, were sent to change the System Fault Protection (SFP) to turn off the LGA-2 (Low Gain Antenna #2) motor if the sequence memory load is terminated. This change prevents a continuous undervoltage situation in the low probability scenario of a relay failure causing a DC bus short circuit while retracting the LGA-2 antenna. The commands were successfully received by the spacecraft (see Special Topic No. 2). 3. On July 20, the Dual Drive Actuator (DDA) pulse/Low Gain Antenna 2 (LGA-2) stow sequence memory load was sent to the spacecraft. The sequence was loaded on the spacecraft without incident (see Special Topic No. 2). 4. On July 20, realtime commands were sent to insert sun gate data into telemetry Map 1 variable Packet No. 9. This change will allow wobble data and sun gate data to be obtained simultaneously during the DDA pulse/LGA-2 stow mini-sequence (see Special Topic No. 2). 5. On July 21, realtime commands were sent to change the System Fault Protection (SFP) AACS-INIT (Attitude and Articulation Control Subsystem) pointing slot from the Earth to the Sun prior to the DDA pulse/LGA-2 stow activities. This change will allow the spacecraft to return to a sun-pointed attitude if an AACS Power on Reset (POR) occurs during DDA pulse/LGA-2 stow activities (see Special Topic No. 2). 6. On July 21, the DDA pulse/LGA-2 stow sequence memory load went active. The warming turn to a 31-degree off-sun attitude commenced at approximately 1757 UTC and completed at 1804 UTC. The first of two motor turn on pulses occurred at 1946 UTC for approximately 2 seconds, as planned. The DDA motor temperature was approximately minus 25 degrees C at turn on. Initial results indicate the motor stalled at 100 milliseconds with inconclusive evidence of ballscrew rotation (see Special Topic No. 2). 7. On July 22, after approximately 24 hours at the warming attitude, the second motor turn on pulse occurred at 1801 UTC for approximately 2 seconds, as planned. The DDA motor temperature was approximately minus 6 degrees C at turn on. Initial results are that the motor stalled at 126 milliseconds indicating some ballscrew rotation occurred. Additionally, the spacecraft under stored sequence control, was commanded back to a 5 degree off-sun attitude at approximately 18:07 UTC. After the sun acquisition, sun gate data was collected to determine if an antenna rib is still obscuring the sun gate signal. Data analysis indicates that the sun gate is still obscured, indicating no ribs released (see Special Topic No. 2). 8. On July 23, the Low Gain Antenna (LGA-2) motors were turned on at approximately 1946 UTC for a duration of 16 seconds to stow the LGA-2 antenna and collect spacecraft dynamics data from the activity. Additionally, realtime commands were sent to perform an open loop wobble compensation. Data analysis is in progress. 9. During the week, the DC bus imbalance reading has continued to change significantly. The DC measurement has ranged from 92DN (10.6 volts) to 151DN (17.8 volts) and now reads 108DN (12.5 volts). This measurement variation is consistent with the model developed by the AC/DC special anomaly team. The AC measurement has remained relatively unchanged and reads 3.1 volts. 10. The Spacecraft status as of July 23, 1992, is as follows: a) System Power Margin - 51 watts b) Spin Configuration - Dual-Spin c) Spin Rate/Sensor - 3.15 rpm/Acquisition Sensor d) Spacecraft Attitude is approximately 5 degrees off-sun (leading) e) Downlink telemetry rate/antenna-40 bps (coded)/LGA-1 f) General Thermal Control - all temperatures within acceptable range g) RPM Tank Pressures - all within acceptable range h) Orbiter Science- UVS, EUV, DDS, MAG, EPD, and HIC are powered on i) Probe/RRH - powered off, temperatures within acceptable range j) CMD Loss Timer Setting - 264 hours Time To Initiation - 263 hours UPLINK GENERATION/COMMAND REVIEW AND APPROVAL: 1. The Dual Drive Actuator (DDA) pulse/LGA-2 stow mini-sequence memory load was approved for transmission by the Project on July 17, 1992. This mini-sequence covers spacecraft activities from July 21, 1992 to July 24, 1992. 2. The EE-7 (Earth-Earth 7) final sequence and command generation package was approved by the Project on July 23, 1992. This sequence covers spacecraft activities from August 10, 1992 to November 23, 1992. TRAJECTORY As of noon Thursday, July 23, 1992, the Galileo Spacecraft trajectory status was as follows: Distance from Earth 125,608,000 miles (1.35 AU) Distance from Sun 166,926,000 miles (1.80 AU) Heliocentric Speed 46,300 miles per hour Distance from Jupiter 670,891,000 miles Round Trip Light Time 22 minutes, 38 seconds SPECIAL TOPIC 1. As of July 23, 1992, a total of 8062 real-time commands have been transmitted to Galileo since Launch. Of these, 3190 were pre-planned in the sequence design and 4872 were not. In the past week, 28 real time commands were transmitted; 25 were pre-planned in the sequence design and 3 were not. In addition, 5453 mini-sequence commands have been transmitted since March 1991; 3201 were pre-planned and 2252 were not. In the past week, 414 mini-sequence commands were transmitted. Major command activities this week included commands to verify the commandability of the spacecraft, update the System Fault Protection (SFP), uplink the DDA pulse/LGA-2 stow sequence memory load, update the telemetry map variable packets, and perform wobble compensation. 2. The High Gain Antenna (HGA) DDA pulse/LGA-2 stow activities are scheduled from July 21 to July 24, 1992. The warming turn to a 31 degree off-sun attitude along with the first DDA two second motor turn on was performed on July 21. The spacecraft remained at the warming attitude for approximately 24 hours. The second DDA motor turn on was performed on July 22 just prior to the spacecraft turning back to a 5 degree off-sun attitude. Sun gate data was collected after the sun acquisition completed. The LGA-2 motors were turned on for 16 seconds on July 23 and the LGA-2 antenna was successfully stowed. The star scanner checkout, along with collection of sun gate and wobble data is scheduled during the July 23-24 time period. ___ _____ ___ /_ /| /____/ \ /_ /| Ron Baalke | baalke@kelvin.jpl.nasa.gov | | | | __ \ /| | | | Jet Propulsion Lab | ___| | | | |__) |/ | | |__ M/S 525-3684 Telos | Most of the things you /___| | | | ___/ | |/__ /| Pasadena, CA 91109 | worry about will never |_____|/ |_|/ |_____|/ | happen. ------------------------------ Date: Fri, 24 Jul 92 19:49:25 GMT From: Colby Kraybill Subject: SPIF Update Newsgroups: sci.image.processing,sci.space Space and Planetary Image Facility Update: Currently in the CD-ROM players, The first two disks of the Voyager fly-bys of Saturn. The Viking Thermal Mapper disk. We also try to mirror some of the image processing applications that Ames keeps. They are in pub/ImageProcessing/(platform) For more information concerning SPIF, get the file pub/info/begginer-info -- Colby Kraybill Space and Planetary Image Facility University of New Mexico ------------------------------ Date: 24 Jul 92 16:39:52 GMT From: Richard Murphy Subject: TSS-1 launch time Newsgroups: sci.space TSS-1 is set for launch at 13:56 GMT July 31. The satellite deployment should begin early on Aug. 2. R. Murphy ------------------------------ Date: Sat, 25 Jul 1992 02:26:57 GMT From: TS Kelso Subject: Two-Line Orbital Element Sets, Part 1 Newsgroups: sci.space The most current orbital elements from the NORAD two-line element sets are carried on the Celestial BBS, (513) 427-0674, and are updated daily (when possible). Documentation and tracking software are also available on this system. The Celestial BBS may be accessed 24 hours/day at 300, 1200, 2400, 4800, or 9600 bps using 8 data bits, 1 stop bit, no parity. Element sets (also updated daily) and some documentation and software are available via anonymous ftp from archive.afit.af.mil (129.92.1.66) in the directory pub/space. As a service to the satellite user community, the most current of these elements are uploaded weekly to sci.space.news and rec.radio.amateur.misc. This week's elements are provided below. - Current Two-Line Element Sets #028a - Alouette 1 1 00424U 62B-A 1 92201.56922435 .00000076 00000-0 85852-4 0 5845 2 00424 80.4637 253.2400 0024164 108.4351 251.9424 13.67715658487033 ATS 3 1 03029U 67111 A 92198.51453824 -.00000079 00000-0 99999-4 0 7939 2 03029 14.0749 14.4147 0012686 240.0840 120.0646 1.00272896 90411 Cosmos 398 1 04966U 71 16 A 92205.87593322 .00062193 23810-4 22862-3 0 5681 2 04966 51.4934 247.6121 1645194 325.5041 24.8980 12.44851870681574 Starlette 1 07646U 75010 A 92199.92466238 -.00000195 00000-0 -10515-3 0 4320 2 07646 49.8250 32.7206 0206725 186.7341 173.0762 13.82176587881130 LAGEOS 1 08820U 76039 A 92204.46702458 .00000006 00000-0 99999-4 0 4424 2 08820 109.8451 257.5966 0043482 73.8949 286.6648 6.38664444122784 ETS-2 1 09852U 77014 A 92190.49579743 -.00000259 00000-0 99999-4 0 6793 2 09852 10.8042 50.2349 0005583 264.5924 95.3382 1.00110990 3382 GOES 2 1 10061U 77048 A 92188.52508295 -.00000262 00000-0 99999-4 0 7996 2 10061 9.7843 54.4624 0000923 21.4239 338.5675 1.00272339 56534 IUE 1 10637U 78012 A 92201.64956278 -.00000187 00000-0 99999-4 0 5673 2 10637 33.5054 106.3013 1340744 14.9933 348.6700 1.00227288 5884 GPS-0001 1 10684U 78020 A 92200.99545436 -.00000002 00000-0 99999-4 0 8872 2 10684 64.2114 66.3188 0066826 158.6006 201.7522 1.98070028 91100 GPS-0002 1 10893U 78 47 A 92196.47188783 -.00000016 00000-0 99999-4 0 6466 2 10893 63.9371 306.8225 0202045 13.1596 347.3711 2.01628037103904 GOES 3 1 10953U 78062 A 92203.81265666 .00000100 00000-0 99999-4 0 4600 2 10953 8.7201 56.9649 0004609 76.2173 283.9388 1.00269845 4754 SeaSat 1 1 10967U 78064 A 92203.25128867 .00000187 00000-0 10433-3 0 8475 2 10967 108.0167 101.7301 0001660 269.1291 90.9664 14.37650795736337 GPS-0003 1 11054U 78093 A 92202.51280237 -.00000015 00000-0 99999-4 0 7311 2 11054 63.4813 302.5593 0070978 121.4497 239.3092 2.00575329101018 Nimbus 7 1 11080U 78098 A 92204.21196277 .00000007 00000-0 22066-4 0 9834 2 11080 99.1404 99.6321 0008999 188.9045 171.1950 13.83678903693964 GPS-0004 1 11141U 78112 A 92196.90478285 -.00000002 00000-0 99999-4 0 4466 2 11141 64.2118 66.5057 0049605 23.7546 336.5477 1.92895017 99456 GPS-0005 1 11690U 80 11 A 92204.82594234 -.00000001 00000-0 99999-4 0 3895 2 11690 64.5802 68.2627 0134691 201.1642 158.3619 2.00549924105616 GPS-0006 1 11783U 80 32 A 92113.08123957 -.00000016 00000-0 99999-4 0 6729 2 11783 63.1246 304.4863 0196643 28.9912 332.0945 2.03456675 87966 GOES 5 1 12472U 81049 A 92202.55010292 -.00000243 00000-0 99999-4 0 3428 2 12472 5.3076 66.1500 0003911 353.6111 6.5140 1.00299534 39899 Cosmos 1383 1 13301U 82 66 A 92205.16799452 .00000029 00000-0 26385-4 0 9350 2 13301 82.9320 98.5971 0026185 206.5454 153.4364 13.68014433502535 LandSat 4 1 13367U 82 72 A 92205.70175209 .00000427 00000-0 99999-4 0 3916 2 13367 98.2755 261.7476 0006120 246.0233 114.0323 14.57085155533073 IRAS 1 13777U 83 4 A 92205.55300105 .00000260 00000-0 20278-3 0 1988 2 13777 98.9934 39.2403 0013376 69.4815 290.7783 13.99131465154236 Cosmos 1447 1 13916U 83 21 A 92202.00497842 .00000026 00000-0 21183-4 0 126 2 13916 82.9458 167.3012 0037145 169.3829 190.8115 13.74256832467571 TDRS 1 1 13969U 83 26 B 92201.80865622 .00000126 00000-0 99999-4 0 7185 2 13969 6.2454 58.3959 0003151 34.1142 325.9982 1.00281606 7060 GOES 6 1 14050U 83 41 A 92200.73143279 .00000088 00000-0 99999-4 0 7178 2 14050 4.0782 68.9902 0001411 312.1590 47.8406 1.00297439 5789 OSCAR 10 1 14129U 83 58 B 92199.99241900 -.00000029 00000-0 99998-4 0 8826 2 14129 26.6608 73.4038 6036720 1.1541 359.9406 2.05881926 40414 GPS-0008 1 14189U 83 72 A 92205.01361620 -.00000003 00000-0 99999-4 0 2503 2 14189 63.7911 63.8307 0136707 231.3048 127.5386 2.00563300 66142 LandSat 5 1 14780U 84 21 A 92205.67762391 .00000147 00000-0 37634-4 0 1939 2 14780 98.1868 265.3967 0001624 235.3914 124.7134 14.57128295446482 UoSat 2 1 14781U 84 21 B 92198.58455609 .00000478 00000-0 86059-4 0 2902 2 14781 97.8477 233.2242 0012516 354.9765 5.1315 14.68610507447454 GPS-0009 1 15039U 84 59 A 92202.69793237 -.00000004 00000-0 99999-4 0 6200 2 15039 63.5436 62.9052 0039728 218.8971 140.8910 2.00569471 59377 Cosmos 1574 1 15055U 84 62 A 92204.51195297 .00000030 00000-0 26310-4 0 2343 2 15055 82.9567 217.3088 0028193 353.5199 6.5588 13.73557114405268 GPS-0010 1 15271U 84 97 A 92205.13090864 -.00000015 00000-0 99999-4 0 3117 2 15271 62.7728 300.9956 0123153 339.4391 20.1146 2.00562057 56539 Cosmos 1602 1 15331U 84105 A 92205.53379181 .00000983 00000-0 11691-3 0 9009 2 15331 82.5322 6.7336 0020697 338.2622 21.7706 14.83283538421647 NOAA 9 1 15427U 84123 A 92204.42273467 .00000306 00000-0 18330-3 0 1370 2 15427 99.1414 232.1854 0015374 20.2870 339.8908 14.13417389392198 GPS-0011 1 16129U 85 93 A 92204.85590601 -.00000003 00000-0 99999-4 0 89 2 16129 64.3139 64.4704 0127661 143.7812 217.1671 2.00565392 49731 Mir 1 16609U 86 17 A 92205.84149550 .00014105 00000-0 22900-3 0 4507 2 16609 51.6250 63.4571 0002810 325.6111 34.4801 15.53001704367988 SPOT 1 1 16613U 86 19 A 92205.53750589 .00000070 00000-0 42051-4 0 7565 2 16613 98.7154 278.4085 0002276 102.2810 257.8629 14.20033699 18115 Cosmos 1766 1 16881U 86 55 A 92200.08536611 .00001045 00000-0 12709-3 0 7508 2 16881 82.5189 70.2051 0021240 14.8569 345.3331 14.82405165321842 EGP 1 16908U 86 61 A 92193.43954910 -.00000025 00000-0 99999-4 0 5795 2 16908 50.0139 94.1317 0011113 322.4175 37.5847 12.44404413268894 NOAA 10 1 16969U 86 73 A 92205.05225017 .00000299 00000-0 14501-3 0 9797 2 16969 98.5332 223.5539 0013029 189.5559 170.5343 14.24687846303761 MOS-1 1 17527U 87 18 A 92205.71878898 .00000112 00000-0 96551-4 0 2290 2 17527 99.0296 275.0132 0000680 81.4061 278.7178 13.94907974276269 GOES 7 1 17561U 87 22 A 92203.47679693 -.00000026 00000-0 99999-4 0 1110 2 17561 0.0232 265.9190 0001089 255.6433 198.4488 1.00272859 3006 Kvant-1 1 17845U 87 30 A 92204.94061461 .00008153 00000-0 13577-3 0 502 2 17845 51.6248 67.9435 0002852 324.9459 35.1841 15.52966534367846 DMSP B5D2-3 1 18123U 87 53 A 92203.84694091 -.00000019 00000-0 99999-7 0 5219 2 18123 98.8030 34.2833 0014519 7.5146 352.6315 14.15163048262650 RS-10/11 1 18129U 87 54 A 92205.47282882 .00000176 00000-0 18085-3 0 2851 2 18129 82.9290 121.5779 0012158 143.6087 216.5880 13.72290698254762 Meteor 2-16 1 18312U 87 68 A 92203.60605596 .00000070 00000-0 57458-4 0 8895 2 18312 82.5510 43.4955 0010967 267.8050 92.1854 13.83954788248840 Meteor 2-17 1 18820U 88 5 A 92203.16466735 .00000107 00000-0 89894-4 0 7374 2 18820 82.5443 102.2180 0017122 341.6508 18.4043 13.84644052226031 DMSP B5D2-4 1 18822U 88 6 A 92204.91598510 .00000066 00000-0 37687-4 0 4215 2 18822 98.5357 74.1300 0005852 198.7702 161.3295 14.22682556231799 Glonass 34 1 19163U 88 43 A 92199.75401626 .00000018 00000-0 99999-4 0 5303 2 19163 64.9324 133.8282 0007177 197.4246 162.5471 2.13102112 31757 Glonass 36 1 19165U 88 43 C 92194.64823847 .00000018 00000-0 99999-4 0 7785 2 19165 64.9182 133.9847 0004667 326.0425 33.9005 2.13102517 32269 METEOSAT 3 1 19215U 88 51 A 92200.31395474 -.00000258 00000-0 99999-4 0 4438 2 19215 0.3115 42.9199 0002713 176.5948 140.4211 1.00265520 2980 AO-13 1 19216U 88 51 B 92194.98725910 -.00637148 00000-0 -31247+1 0 4338 2 19216 57.1350 13.9049 7356190 289.9866 10.5842 2.09091985 31295 OKEAN 1 1 19274U 88 56 A 92200.38449610 .00000652 00000-0 81859-4 0 4531 2 19274 82.5147 169.0487 0020596 142.1656 218.1010 14.81318679217599 Meteor 3-2 1 19336U 88 64 A 92191.85818953 .00000031 00000-0 67108-4 0 9414 2 19336 82.5429 104.1988 0015865 232.6700 127.2976 13.16949449190150 Glonass 39 1 19503U 88 85 C 92205.46278038 -.00000021 00000-0 99999-4 0 7815 2 19503 65.6547 12.6762 0006146 176.1164 183.9118 2.13102627 29983 NOAA 11 1 19531U 88 89 A 92204.42899118 .00000089 00000-0 58509-4 0 8763 2 19531 99.0848 168.5706 0011109 289.0142 70.9823 14.12716973197119 TDRS 2 1 19548U 88 91 B 92198.35589089 -.00000256 00000-0 99999-4 0 4447 2 19548 0.6180 77.2426 0003762 47.4310 235.3689 1.00259308 1330 Glonass 40 1 19749U 89 1 A 92203.62723596 .00000018 00000-0 00000+0 0 6922 2 19749 64.8636 133.3332 0006523 272.8212 87.1113 2.13102094 27476 Glonass 41 1 19750U 89 1 B 92204.15389974 .00000018 00000-0 00000+0 0 7449 2 19750 64.8922 133.3342 0007055 255.6278 104.2954 2.13102401 27486 GPS BII-01 1 19802U 89 13 A 92204.70837093 .00000016 00000-0 99999-4 0 4435 2 19802 55.0326 167.1908 0042140 172.6988 187.3515 2.00558738 25125 Akebono 1 19822U 89 16 A 92205.06550039 .00011172 00000-0 72054-3 0 5609 2 19822 75.0911 205.9963 3933776 69.8841 327.7031 7.55507051 55991 Meteor 2-18 1 19851U 89 18 A 92203.83951230 .00000042 00000-0 32107-4 0 6896 2 19851 82.5193 338.2651 0015559 20.9244 339.2551 13.84291974171485 MOP-1 1 19876U 89 20 B 92200.18014710 .00000012 00000-0 99999-4 0 3935 2 19876 0.2411 349.2189 0002581 128.6405 242.1275 1.00273036 8361 TDRS 3 1 19883U 89 21 B 92199.29362206 -.00000239 00000-0 99999-4 0 4572 2 19883 0.0678 81.5810 0002782 300.5366 337.9413 1.00268878 82489 GPS BII-02 1 20061U 89 44 A 92204.54625266 -.00000033 00000-0 99999-4 0 4471 2 20061 54.9083 344.7350 0108306 194.5011 165.1989 2.00562241 22864 Nadezhda 1 1 20103U 89 50 A 92203.18305642 .00000038 00000-0 33823-4 0 5881 2 20103 82.9600 81.0235 0039080 67.8231 292.7064 13.73791405152748 GPS BII-03 1 20185U 89 64 A 92204.88243690 .00000016 00000-0 99999-4 0 3945 2 20185 54.8793 167.9195 0012573 198.6760 161.2614 2.00558686 21449 -- Dr TS Kelso Assistant Professor of Space Operations tkelso@afit.af.mil Air Force Institute of Technology ------------------------------ Date: 24 Jul 92 16:00:49 GMT From: Mike McCants Subject: Wanted satellite tracking program for GPS sats Newsgroups: sci.space In article <1402@lewis.OZ> steve@lewis.OZ (Steve Pattinson) writes: >Can anybody please tell me where I can get a satellite tracking program >suitable for use with GPS satellites. I'm sure I can fix up a program to do what you want - no charge. >Please don't e-mail me - incoming messages are broke! My user name on Celestial is Mike McCants. My email address is mike@comshare.com. ------------------------------ End of Space Digest Volume 15 : Issue 037 ------------------------------