Date: Thu, 2 Dec 93 04:30:45 PST From: Ham-Space Mailing List and Newsgroup <ham-space@ucsd.edu> Errors-To: Ham-Space-Errors@UCSD.Edu Reply-To: Ham-Space@UCSD.Edu Precedence: Bulk Subject: Ham-Space Digest V93 #97 To: Ham-Space Ham-Space Digest Thu, 2 Dec 93 Volume 93 : Issue 97 Today's Topics: (none) What are Global Positioning satellite frequencies? Send Replies or notes for publication to: <Ham-Space@UCSD.Edu> Send subscription requests to: <Ham-Space-REQUEST@UCSD.Edu> Problems you can't solve otherwise to brian@ucsd.edu. Archives of past issues of the Ham-Space Digest are available (by FTP only) from UCSD.Edu in directory "mailarchives/ham-space". We trust that readers are intelligent enough to realize that all text herein consists of personal comments and does not represent the official policies or positions of any party. Your mileage may vary. So there. ---------------------------------------------------------------------- Date: 1 Dec 93 16:13:54 GMT From: news-mail-gateway@ucsd.edu Subject: (none) To: ham-space@ucsd.edu Satellite: INTELSAT 5 F-2 Catalog number: 12089 Epoch time: 93316.34011391 Element set: 507 Inclination: 4.4833 deg RA of node: 65.5032 deg Eccentricity: 0.0004321 Arg of perigee: 167.1666 deg Mean anomaly: 279.9183 deg Mean motion: 1.00268695 rev/day Decay rate: -1.37E-06 rev/day^2 Epoch rev: 1005 Checksum: 273 Satellite: INTELSAT 5 F-3 Catalog number: 12994 Epoch time: 93318.41247243 Element set: 112 Inclination: 4.1234 deg RA of node: 66.3660 deg Eccentricity: 0.0003531 Arg of perigee: 163.7862 deg Mean anomaly: 154.9332 deg Mean motion: 1.00277097 rev/day Decay rate: 9.9E-07 rev/day^2 Epoch rev: 823 Checksum: 276 Satellite: INTELSAT 5 F-6 Catalog number: 14077 Epoch time: 93318.45390750 Element set: 612 Inclination: 2.5633 deg RA of node: 71.2496 deg Eccentricity: 0.0003338 Arg of perigee: 167.6751 deg Mean anomaly: 287.9989 deg Mean motion: 1.00266681 rev/day Decay rate: -2.55E-06 rev/day^2 Epoch rev: 586 Checksum: 318 Satellite: INTELSAT 5 F-8 Catalog number: 14786 Epoch time: 93320.65803884 Element set: 521 Inclination: 2.2639 deg RA of node: 72.2290 deg Eccentricity: 0.0003383 Arg of perigee: 160.8112 deg Mean anomaly: 239.5413 deg Mean motion: 1.00273816 rev/day Decay rate: 7.9E-07 rev/day^2 Epoch rev: 3645 Checksum: 286 Satellite: INTELSAT 5A F-11 Catalog number: 15873 Epoch time: 93324.30626863 Element set: 220 Inclination: 0.7736 deg RA of node: 77.9886 deg Eccentricity: 0.0003287 Arg of perigee: 154.8030 deg Mean anomaly: 113.8487 deg Mean motion: 1.00274405 rev/day Decay rate: 6.1E-07 rev/day^2 Epoch rev: 538 Checksum: 288 Satellite: INTELSAT 5A F-12 Catalog number: 16101 Epoch time: 93320.10528561 Element set: 518 Inclination: 0.2128 deg RA of node: 86.6661 deg Eccentricity: 0.0002379 Arg of perigee: 150.7203 deg Mean anomaly: 214.8430 deg Mean motion: 1.00275169 rev/day Decay rate: 1.8E-07 rev/day^2 Epoch rev: 1214 Checksum: 242 Satellite: INTELSAT 5A F-13 Catalog number: 19121 Epoch time: 93317.04756235 Element set: 420 Inclination: 0.0109 deg RA of node: 220.7814 deg Eccentricity: 0.0001801 Arg of perigee: 22.8621 deg Mean anomaly: 132.7088 deg Mean motion: 1.00271401 rev/day Decay rate: -2.57E-06 rev/day^2 Epoch rev: 707 Checksum: 233 Satellite: INTELSAT 6 F-3 Catalog number: 20523 Epoch time: 93321.95100523 Element set: 316 Inclination: 0.0147 deg RA of node: 336.3972 deg Eccentricity: 0.0000655 Arg of perigee: 259.3126 deg Mean anomaly: 129.1493 deg Mean motion: 1.00268888 rev/day Decay rate: -2.13E-06 rev/day^2 Epoch rev: 649 Checksum: 391 Satellite: INTELSAT VI F4 Catalog number: 20667 Epoch time: 93320.68614126 Element set: 613 Inclination: 0.0125 deg RA of node: 338.8919 deg Eccentricity: 0.0001558 Arg of perigee: 220.1098 deg Mean anomaly: 163.7843 deg Mean motion: 1.00271848 rev/day Decay rate: 7.5E-07 rev/day^2 Epoch rev: 580 Checksum: 274 Satellite: INTELSAT 6 F-5 Catalog number: 21653 Epoch time: 93322.14714462 Element set: 513 Inclination: 0.0124 deg RA of node: 25.2846 deg Eccentricity: 0.0000851 Arg of perigee: 210.3324 deg Mean anomaly: 210.0842 deg Mean motion: 1.00270135 rev/day Decay rate: -1.59E-06 rev/day^2 Epoch rev: 829 Checksum: 351 Satellite: INTELSAT VI-F1 Catalog number: 21765 Epoch time: 93323.47277801 Element set: 515 Inclination: 0.0055 deg RA of node: 207.3684 deg Eccentricity: 0.0000992 Arg of perigee: 16.8105 deg Mean anomaly: 337.0362 deg Mean motion: 1.00269796 rev/day Decay rate: -1.77E-06 rev/day^2 Epoch rev: 746 Checksum: 277 Satellite: INTELSAT K Catalog number: 21989 Epoch time: 93321.92928887 Element set: 418 Inclination: 0.0634 deg RA of node: 82.7189 deg Eccentricity: 0.0001540 Arg of perigee: 171.1641 deg Mean anomaly: 116.1202 deg Mean motion: 1.00269461 rev/day Decay rate: -1.41E-06 rev/day^2 Epoch rev: 1591 Checksum: 266 ------------------------------ Date: 1 Dec 93 09:19:44 GMT From: ogicse!emory!europa.eng.gtefsd.com!howland.reston.ans.net!cs.utexas.edu!not-for-mail@network.ucsd.edu Subject: What are Global Positioning satellite frequencies? To: ham-space@ucsd.edu Path: news.csuohio.edu!usenet.ins.cwru.edu!howland.reston.ans.net!cs.utexas.edu!not-for-mail From: bmm1@freenet.scri.fsu.edu (Bruce M. Marshall) Newsgroups: rec.radio.scanner Subject: What are Global Positioning satellite frequencies? Date: 1 Dec 1993 14:34:05 -0600 Organization: UTexas Mail-to-News Gateway Lines: 13 Sender: daemon@cs.utexas.edu Message-ID: <199312012033.AA15653@freenet2.scri.fsu.edu> NNTP-Posting-Host: news.cs.utexas.edu Does anyone know where I can get technical data on the global positioning system satellites? Specifically I would like to know their frequencies, modulation type, data format and how many of them are presently in orbit. It would also be interesting to know their norad designation, orbital elements and some spacecraft statistics like power source and rf transmit power. I have found lots of information on how to use the equipment but nothing technical on the whole system. thanks. -- Bruce M. Marshall bmm1@freenet.fsu.edu voice 615 481 0990 fax 615 481 8039 ------------------------------ End of Ham-Space Digest V93 #97 ****************************** ******************************