USA Space Debris Environment and Operational Updates
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OSTM/Jason-2 Products Handbook
OSTM/Jason-2 Products Handbook References: CNES : SALP-MU-M-OP-15815-CN EUMETSAT : EUM/OPS-JAS/MAN/08/0041 JPL: OSTM-29-1237 NOAA : Issue: 1 rev 0 Date: 17 June 2008 OSTM/Jason-2 Products Handbook Iss :1.0 - date : 17 June 2008 i.1 Chronology Issues: Issue: Date: Reason for change: 1rev0 June 17, 2008 Initial Issue People involved in this issue: Written by (*) : Date J.P. DUMONT CLS V. ROSMORDUC CLS N. PICOT CNES S. DESAI NASA/JPL H. BONEKAMP EUMETSAT J. FIGA EUMETSAT J. LILLIBRIDGE NOAA R. SHARROO ALTIMETRICS Index Sheet : Context: Keywords: Hyperlink: OSTM/Jason-2 Products Handbook Iss :1.0 - date : 17 June 2008 i.2 List of tables and figures List of tables: Table 1 : Differences between Auxiliary Data for O/I/GDR Products 1 Table 2 : Summary of error budget at the end of the verification phase 9 Table 3 : Main features of the OSTM/Jason-2 satellite 11 Table 4 : Mean classical orbit elements 16 Table 5 : Orbit auxiliary data 16 Table 6 : Equator Crossing Longitudes (in order of Pass Number) 18 Table 7 : Equator Crossing Longitudes (in order of Longitude) 19 Table 8 : Models and standards 21 Table 9 : CLS01 MSS model characteristics 22 Table 10 : CLS Rio 05 MDT model characteristics 23 Table 11 : Recommended editing criteria 26 Table 12 : Recommended filtering criteria 26 Table 13 : Recommended additional empirical tests 26 Table 14 : Main characteristics of (O)(I)GDR products 40 Table 15 - Dimensions used in the OSTM/Jason-2 data sets 42 Table 16 - netCDF variable type 42 Table 17 - Variable’s attributes 43 List of figures: Figure 1 -
Handbookhandbook Mobile-Satellite Service (MSS) Handbook
n International Telecommunication Union Mobile-satellite service (MSS) HandbookHandbook Mobile-satellite service (MSS) Handbook *00000* Edition 2002 Printed in Switzerland Geneva, 2002 ISBN 92-61-09951-3 Radiocommunication Bureau Edition 2002 THE RADIOCOMMUNICATION SECTOR OF ITU The role of the Radiocommunication Sector is to ensure the rational, equitable, efficient and economical use of the radio-frequency spectrum by all radiocommunication services, including satellite services, and carry out studies without limit of frequency range on the basis of which Recommendations are adopted. The regulatory and policy functions of the Radiocommunication Sector are performed by World and Regional Radiocommunication Conferences and Radiocommunication Assemblies supported by Study Groups. Inquiries about radiocommunication matters Please contact: ITU Radiocommunication Bureau Place des Nations CH -1211 Geneva 20 Switzerland Telephone: +41 22 730 5800 Fax: +41 22 730 5785 E-mail: [email protected] Web: www.itu.int/itu-r Placing orders for ITU publications Please note that orders cannot be taken over the telephone. They should be sent by fax or e-mail. ITU Sales and Marketing Division Place des Nations CH -1211 Geneva 20 Switzerland Telephone: +41 22 730 6141 English Telephone: +41 22 730 6142 French Telephone: +41 22 730 6143 Spanish Fax: +41 22 730 5194 Telex: 421 000 uit ch Telegram: ITU GENEVE E-mail: [email protected] The Electronic Bookshop of ITU: www.itu.int/publications ITU 2002 All rights reserved. No part of this publication may be reproduced, by any means whatsoever, without the prior written permission of ITU. International Telecommunication Union HandbookHandbook Mobile-satellite service (MSS) Radiocommunication Bureau Edition 2002 - iii - FOREWORD In today’s world, people have become increasingly mobile in both their work and play. -
Aeronautics and Space Report of the President, 1976 Activities
Aeronautics and Space Report of the President 19 76 Activities NOTE TO READERS: ALL PRINTED PAGES ARE INCLUDED, UNNUMBERED BLANK PAGES DURING SCANNING AND QUALITY CONTROL CHECK HAVE BEEN DELETED Aeronautics and Space Report of the President 1976 Activities National Aeronautics and Space Administration Washington, D.C. 20546 Table of Contents Page Page I. Summary of U.S. Aeronautics and Space Ac- X. National Academy of Sciences, National Acad- tivities of 1976 _________________________ 1 emy .of Engineering, National Research 67 Introduction _ _ _ _ _ _ _ _ _ _ _ _ _ _ __ _ _ _ _ _ __ __ 1 Council _______________________________ Space _______________________________ 1 Introduction _ _ _____ _ ______ __ _ ______ __ 67 Aeronautics __ __________ ____ __________ 4 Aerospace Science _ _ _ __ - _ _ _ __ _ __ _ __ _ - - - 67 The Heritage ________________________ 5 Space Applications .................... 69 .. 70 11. National Aeronautics and Space Administration G Aerospace Engineering _ _ _ _ _ _ _ __ _ _ _ - - - - - 6 Education ____________________-------71 Introduction _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 72 Applications to Earth __________________ 6 XI. Office of Telecommunications Policy __i____-- 10 Introduction __ __ __________ _____ ____ __ 72 Science ______________________________ 72 Space Transportation __________________ 15 International Satellite Systems _____ _ _____ 18 Direct Broadcast Satellites ______________ 72 Space Research and Technology _ _ ___ ____ 73 Tracking and Data Acquisition __________ 19 Frequency Management _____ __ _ __ _ ___ __ 20 Domestic Satellite Applications __________ 73 International Affairs ___________________ 74 User Affairs ________________________ 23 XII. -
Observation of Light Curves of Space Objects Hirohisa Kurosaki Japan
Observation of Light Curves of Space Objects Hirohisa Kurosaki Japan Aerospace Exploration Agency Toshifumi Yanagisawa Japan Aerospace Exploration Agency Atsushi Nakajima Japan Aerospace Exploration Agency Abstract Geostationary orbit and low earth orbit have many artificial satellites, and the accidents of these satellites affect every area such as weather forecasts and communications. In the optical observation, the periodical change of the brightness which is caused by the type and the shape of the satellite is seen. In the case of LEO debris, since the movement is fast, it crosses the field of view in several seconds. We used an observation method to get the data of LEO debris. In case of the GEO debris, the rate of motion is slow in comparison with LEO debris. Fixed stars are observed by the same position on the image when the telescope is operated in sidereal tracking mode. Then, space objects are recorded on the image with streaks of light. In this paper, the observation and the detection method of light curve of geostationary orbit debris are discussed. Observing the changes of the operative satellites with some time intervals may help to detect the abnormalities and accidents of them. 1. INTRODUCTION Artificial satellites that have finished their missions and used rockets are called space debris. Most of them are not under any control. The space debris problem must be solved to perform future space development and maintain safety. Many artificial satellites indispensable for human activities circle the earth. If one of these satellites malfunctions, many human activities are impacted. An artificial satellite is monitored to control its trajectory while it is in operation. -
Estimating Gale to Hurricane Force Winds Using the Satellite Altimeter
VOLUME 28 JOURNAL OF ATMOSPHERIC AND OCEANIC TECHNOLOGY APRIL 2011 Estimating Gale to Hurricane Force Winds Using the Satellite Altimeter YVES QUILFEN Space Oceanography Laboratory, IFREMER, Plouzane´, France DOUG VANDEMARK Ocean Process Analysis Laboratory, University of New Hampshire, Durham, New Hampshire BERTRAND CHAPRON Space Oceanography Laboratory, IFREMER, Plouzane´, France HUI FENG Ocean Process Analysis Laboratory, University of New Hampshire, Durham, New Hampshire JOE SIENKIEWICZ Ocean Prediction Center, NCEP/NOAA, Camp Springs, Maryland (Manuscript received 21 September 2010, in final form 29 November 2010) ABSTRACT A new model is provided for estimating maritime near-surface wind speeds (U10) from satellite altimeter backscatter data during high wind conditions. The model is built using coincident satellite scatterometer and altimeter observations obtained from QuikSCAT and Jason satellite orbit crossovers in 2008 and 2009. The new wind measurements are linear with inverse radar backscatter levels, a result close to the earlier altimeter high wind speed model of Young (1993). By design, the model only applies for wind speeds above 18 m s21. Above this level, standard altimeter wind speed algorithms are not reliable and typically underestimate the true value. Simple rules for applying the new model to the present-day suite of satellite altimeters (Jason-1, Jason-2, and Envisat RA-2) are provided, with a key objective being provision of enhanced data for near-real- time forecast and warning applications surrounding gale to hurricane force wind events. Model limitations and strengths are discussed and highlight the valuable 5-km spatial resolution sea state and wind speed al- timeter information that can complement other data sources included in forecast guidance and air–sea in- teraction studies. -
Dear Dr. Saverio Mori, Thank You Very Much for Kindly Inviting Us To
Dear Dr. Saverio Mori, Thank you very much for kindly inviting us to submit a revised manuscript titled “Simulating precipitation radar observations from a geostationary satellite” to Atmospheric Measurement Techniques. We would also appreciate the time and effort you and the reviewers have dedicated to providing insightful feedback on the ways to strengthen our paper. We would like to submit our revised manuscript. We have incorporated changes that reflect the suggestions you and the reviewers have provided. We hope that the revisions properly address the suggestions and comments. Sincerely, A. Okazaki, T. Honda, S. Kotsuki, M. Yamaji, T. Kubota, R. Oki, T. Iguchi, and T. Miyoshi The reviewer comments are in blue and italic and the replies are in black. Anonymous Referee #1 The manuscript presents the usefulness of a “feasible” Ku-band precipitation radar for a geostationary satellite (GeoSat/PR). It is an effort ongoing at JAXA to overcome two limitations of orbiting radar-based systems such as TRMM or GPM, namely, the limited swath and revisit time. A geostationary satellite needs a larger antenna than TRMM PR and GPM KuPR. A 20-m antenna for a 20 km footprint is considered in the study for its feasibility. The scan of the radar is within 6◦ that makes measurements available for a circular disk with a diameter of 8400 km. Effects of Non Uniform Beam Filling (NUBF) and clutter are presented usng an extremely simple cloud model. The impact of coarse resolutions of the GeoSat/PR is quantified on 3-D Typhoon observations obtained with realistic simulations. The subject of is important and the manuscript is, in general, well written. -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
Toward 1-Mgal Accuracy in Global Marine Gravity from Cryosat-2, Envisat, and Jason-1
SPECIALGravity SECTION: and G rpotential a v i t y and fieldspotential fields Toward 1-mGal accuracy in global marine gravity from CryoSat-2, Envisat, and Jason-1 DAVID SANDWELL and EMMANUEL GARCIA, Scripps Institution of Oceanography KHALID SOOFI, ConocoPhillips PAUL WESSEL and MICHAEL CHANDLER, University of Hawaii at Mānoa WALTER H. F. SMITH, National Oceanic and Atmospheric Administration ore than 60% of the Earth’s land and shallow contribution to gravity field improvement, especially Mmarine areas are covered by > 2 km of sediments in the Arctic where the closely spaced repeat tracks can and sedimentary rocks, with the thickest accumulations collect data over unfrozen areas as the ice cover changes on rifted continental margins (Figure 1). Free-air marine (Childers et al., 2012). gravity anomalies derived from Geosat and ERS-1 satellite 3) The Jason-1 satellite was launched in 2001 to replace the altimetry (Fairhead et al., 2001; Sandwell and Smith, 2009; aging Topex/Poseidon satellite. To avoid a potential colli- Andersen et al., 2009) outline most of these major basins sion between Jason 1 and Topex, the Jason-1 satellite was with remarkable precision. Moreover, gravity and bathymetry moved into a lower orbit with a long repeat time of 406 data derived from altimetry are used to identify current and days resulting in an average ground-track spacing of 3.9 paleo-submarine canyons, faults, and local recent uplifts. km at the equator. The maneuver was performed in May These geomorphic features provide clues to where to look 2012 and the satellite is collecting a tremendous new data for large deposits of sediments. -
Space Debris
IADC-11-04 April 2013 Space Debris IADC Assessment Report for 2010 Issued by the IADC Steering Group Table of Contents 1. Foreword .......................................................................... 1 2. IADC Highlights ................................................................ 2 3. Space Debris Activities in the United Nations ................... 4 4. Earth Satellite Population .................................................. 6 5. Satellite Launches, Reentries and Retirements ................ 10 6. Satellite Fragmentations ................................................... 15 7. Collision Avoidance .......................................................... 17 8. Orbital Debris Removal ..................................................... 18 9. Major Meetings Addressing Space Debris ........................ 20 Appendix: Satellite Break-ups, 2000-2010 ............................ 22 IADC Assessment Report for 2010 i Acronyms ADR Active Debris Removal ASI Italian Space Agency CNES Centre National d’Etudes Spatiales (France) CNSA China National Space Agency CSA Canadian Space Agency COPUOS Committee on the Peaceful Uses of Outer Space, United Nations DLR German Aerospace Center ESA European Space Agency GEO Geosynchronous Orbit region (region near 35,786 km altitude where the orbital period of a satellite matches that of the rotation rate of the Earth) IADC Inter-Agency Space Debris Coordination Committee ISRO Indian Space Research Organization ISS International Space Station JAXA Japan Aerospace Exploration Agency LEO Low -
Press Kit , Project ~Arisat-B RELEASE NO: 7643
! News National Aeronautics and Space Administration Washrngton. D.C.20546 AC 202 755-8370 * For Release IMMEDIATE Press Kit , Project ~arisat-B RELEASE NO: 7643 Contents , GENERAL RE&EASE........:.....e...................... 1-3 DELTA LAUNCH VEHICLEoooo...o........oom....a...o.o. 4 STRAIGH$-SIGHT DELTA FACTS AND FIGURES. ............ 5-6 TYPICAL LAUNCH SEQUENCE FOR MARISAT-B ...............7-8 LAUNCH OP&~TIONS,..........................:...... 9 'NASA TEAM...................^.^..^.^.^..^.^^^ 9-10 COMSAT GENERAL CORP.,.............................. 11 ---- ---- -- -- - - -- - - - - - - .- (111SA-lleus-Release-76-83) . NASA TOLAUNCH SECOND BABISAT POB COBSAT GENERAL COOP- (NASA) 12 p Unclas 43127 N!News National Aeronautics and Space Administration' .> t r I Washington, 0.C.20546 I) AC 202 755-8310 For Release: ' Bill O'bonnell Headquarters, Washington, D.C. IMMEDIATE (Phone: 202/73518487) .. +. 4.: RELEASE NO: 76-83 NASA TO LAUNCH SECOND .~RISATFOR COMSAT GENBRAL,CORP. The 98cond maritime satellite (Marisat) will be launched a ,' by NASA for COMSAT General Corp. from Cape Canaveral, Fla., about May 27. 1, The spacecraft will be the second in the new Marisat system designed to provide communications t6 the :u.s. Navy, commercial shipping and offshore industries. I , Marisat-B will be il'alaced into synchronous orbit. over' the equator above the Pacific Ocean at 176.5 degrees W, longitude just west of Hawaii. A third Marisat has been t built as a spare. The first spacecraft, Marisat-1, was launched success- fully Feb. 19 on a Delta vehicle and is in orbit over the Atlantic at 15 degrees W. longitude, where it has been pro- viding service on UHF frequencies to the Navy since March 25. -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Classification of Geosynchronous Objects
esoc European Space Operations Centre Robert-Bosch-Strasse 5 D-64293 Darmstadt Germany T +49 (0)6151 900 www.esa.int CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Produced with the DISCOS Database Prepared by ESA’s Space Debris Office Reference GEN-DB-LOG-00211-OPS-GR Issue 20 Revision 0 Date of Issue 28 May 2018 Status Issued Document Type Technical Note Distribution ESA UNCLASSIFIED - Limited Distribution European Space Agency Agence spatiale europeenne´ Abstract This is a status report on geosynchronous objects as of 1 January 2018. Based on orbital data in ESA’s DISCOS database and on orbital data provided by KIAM the situation near the geostationary ring is analysed. From 1523 objects for which orbital data are available (of which 0 are outdated, i.e. the last available state dates back to 180 or more days before the reference date), 519 are actively controlled, 795 are drifting above, below or through GEO, 189 are in a libration orbit and 19 are in a highly inclined orbit. For 1 object the status could not be determined. Furthermore, there are 59 uncontrolled objects without orbital data (of which 54 have not been cata- logued). Thus the total number of known objects in the geostationary region is 1582. If you detect any error or if you have any comment or question please contact: Stijn Lemmens European Space Agency European Space Operations Center Space Debris Office (OPS-GR) Robert-Bosch-Str. 5 64293 Darmstadt, Germany Tel.: +49-6151-902634 E-mail: [email protected] Page 1 / 187 European Space Agency CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Agence spatiale europeenne´ Date 28 May 2018 Issue 20 Rev 0 Table of contents 1 Introduction 3 2 Sources 4 2.1 USSTRATCOM Two-Line Elements (TLEs) .