Information furnished in conformity with the Convention on Registration of Objects Launched into Outer Space
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1 United Nations Secretariat Distr.: General 4 August 2008 English Original: [Start1] Committee on the Peaceful Uses of Outer Space Information furnished in conformity with the Convention on Registration of Objects Launched into Outer Space Note verbale dated 16 July 2008 from the Permanent Mission of France to the United Nations (Vienna) addressed to the Secretary-General The Permanent Mission of France to the United Nations (Vienna) presents its compliments to the Secretary-General of the United Nations and, in accordance with article IV of the Convention on Registration of Objects Launched into Outer Space (General Assembly resolution 3235 (XXIX), annex), has the honour to submit information on space objects launched by France during the period from 1 August to 31 December (annex I), information on space objects registered by France that have re-entered the Earth s atmosphere during that period (annex II) and supplementary information on France s previously launched space objects (annex III). V (E) * *
2 2 Annex I Registration data on space objects launched by France between 1 August and 31 December * Basic orbital characteristics Remarks Registration number Date of launch Launch site Type of launcher Nodal period (minutes) Inclination (degrees) Apogee (km) Perigee (km) General function of space object Ariane launch number Satellite launched by launcher State/ organization -032A 4 August Baikonur, Kazakhstan Proton HotBird 8 telecommunications satellite -033B 11 August Syracuse 3B telecommunications satellite -033C 11 August SYLDA intersatellite structure V 172 Syracuse 3B JCSAT 10 France Japan -033D 11 August ESC A cryogenic upper stage -043D 13 October -043E 13 October SYLDA intersatellite structure ESC A cryogenic upper stage V 173 DIRECTV 9S OPTUS D1 LDREX 2 United States Australia Japan -054C 8 December -054D 8 December SYLDA intersatellite structure ESC A cryogenic upper stage V 174 WILDBLUE 1 AMC-18 United States United States * The registration data are reproduced in the form in which they were received.
3 Basic orbital characteristics Remarks Registration number Date of launch Launch site Type of launcher Nodal period (minutes) Inclination (degrees) Apogee (km) Perigee (km) General function of space object Ariane launch number Satellite launched by launcher State/ organization -063A 27 December Baikonur, Kazakhstan Soyuz- 2.1b Convection, Rotation and Planetary Transits (COROT) exoplanet research satellite (see below) Note: France registers European Telecommunications Satellite Organization (EUTELSAT) satellites. 3 Convection, Rotation and Planetary Transits satellite (COROT) Name of space object: Convection, Rotation and Planetary Transits satellite (COROT) International designator: -063A Name of launching authority: Centre national d études spatiales (CNES) Date of launch: 27 December Location of launch site: Baikonur, Kazakhstan Launch vehicle: Soyuz-2.1b (14A14) No. 001 with Fregat upper stage (No. 1013) Basic orbital characteristics: Nodal period: 103 minutes Inclination: 90 Apogee: 906 km Perigee: 895 km Geostationary orbital position: Not applicable General description of the space object: COROT is a satellite designed for extrasolar planet research. Its payload (289 kg) consists of the Corotel afocal telescope, the Corotcam camera, the Corotcase equipment bay, and the Corotlog flight software. COROT uses the Alcatel Alenia Space Proteus platform.
4 4 Frequency plan: The scientific mission has two objectives: to study the internal structure of stars (seismology) and to detect exoplanets using the transit method, which involves observing tiny variations in a star s brightness, indicating that a planet is crossing in front of the star s disk. Earth-space: MHz (telecommand) Space-Earth: MHz (telemetry) Lifetime: 3 years (nominal period)
5 Annex II Information provided by France in conformity with article IV, paragraph 3, of the Convention on Registration of Objects Launched into Outer Space on space objects registered by France that re-entered the Earth s atmosphere between 1 August and 31 December * Registration number Date of launch General function of space object Atmospheric re-entry F 29 October 1991 Non-functional launcher element 8 October 5 * The data are reproduced in the form in which they were received.
6 6 Annex III Additional information provided by France in conformity with article IV, paragraph 2, of the Convention on Registration of Objects Launched into Outer Space on space objects registered by France * Table 1 satellites in an inclined orbit and still operational Registration number Satellite Type of orbit A SPOT 2 Earth observation satellite 800 km sun-synchronous A Helios 1A space-object technique and technology research satellite 625 km polar orbit A SPOT 4 Earth observation satellite 800 km sun-synchronous A SPOT 5 Earth observation satellite 800 km sun-synchronous C DEMETER scientific satellite 715 km polar orbit A Helios IIA observation satellite 670 km polar orbit C Essaim 1 satellite for characterization of Earth s electromagnetic 660 km polar orbit environment D Essaim 2 satellite for characterization of Earth s electromagnetic 660 km polar orbit environment E Essaim 3 satellite for characterization of Earth s electromagnetic 660 km polar orbit environment F Essaim 4 satellite for characterization of Earth s electromagnetic 660 km polar orbit environment G PARASOL satellite for characterization of the radiative and microphysical 705 km polar orbit properties of clouds and aerosols -016B CALIPSO satellite for three-dimensional characterization of clouds and 705 km polar orbit aerosols -063A COROT satellite for exoplanet research 906 km polar orbit * The data are reproduced in the form in which they were received.
7 Table 2 satellites in geostationary orbit and still operational, with approximate orbital positions Registration number Satellite Approximate orbital position as at 31 December B EUTELSAT II F2 telecommunications satellite 48.0 E A EUTELSAT II F3 telecommunications satellite 21.5 E B HotBird 1 telecommunications satellite 13.0º E A TC 2C telecommunications satellite 5.2º W B TC 2D telecommunications satellite 8.0º W A HotBird 2 telecommunications satellite 13.0 E A HotBird 3 telecommunications satellite 13.0º E A HotBird 4 telecommunications satellite 13.0º E A EUTELSAT W2 telecommunications satellite 16.0º E A EUTELSAT W3 telecommunications satellite 7.0º E A SESAT 1 telecommunications satellite 36.0º E A EUTELSAT W4 telecommunications satellite 36.0º E A EUTELSAT W1 telecommunications satellite 10.0º E A Eurobird 1 telecommunications satellite 28.5º E A Atlantic Bird 2 telecommunications satellite 8.0º W A Atlantic Bird 3 telecommunications satellite 5.0º W A HotBird 6 telecommunications satellite 13.0º E A Atlantic Bird 1 telecommunications satellite 12.5º W A EUTELSAT W5 telecommunications satellite 70.5º E A E-Bird telecommunications satellite 33º E A W3A telecommunications satellite 7º E B Syracuse 3A telecommunications satellite not available -007B HotBird 7A telecommunications satellite 13º E -032A HotBird 8 telecommunications satellite 13º E 7
8 8 Table 3 satellites still in orbit but no longer operational Registration number Satellite A A1 experimental satellite A FR1 technological satellite A D1 experimental satellite A Diadème 1 experimental satellite A Diadème 2 experimental satellite A Symphonie 1 experimental telecommunications satellite A COS B scientific satellite A Symphonie 2 experimental telecommunications satellite A Meteosat 1 meteorological satellite A OTS 2 experimental telecommunications satellite A GEOS 2 scientific satellite B TC 1A telecommunications satellite Two reorbiting manoeuvres effected on 7 and 8 September 1992 from orbital position 11º W. Final orbit: apogee: 42,595 km, eccentricity: 1.3*10-3, perigee: +375 km above the GSO orbit; drift 5.3º/day to west. Satellite finally ceased operation on 9 September B TC 1B telecommunications satellite Attitude and orbit control system supply breakdown on 15 January 1988 (last orbital position: 5º W); the satellite is rotating around its principal inertia axis Z; oscillation orbit about 75º W A SPOT 1 Earth observation satellite In conformity with the Inter-Agency Space Debris Coordination Committee (IADC) recommendations, deorbiting manoeuvres were effected in November 2003 to lower the satellite s perigee from 800 to 594 km in order to restrict its life in space to approximately 18 years B EUTELSAT I-F4 (ECS 4) telecommunications satellite B TC 1C telecommunications satellite Two reorbiting manoeuvres 12 hours apart were effected on 9 February 1996 from orbital position 1º E. Final orbit: apogee: 42,830 km, eccentricity: 0.01; perigee: 42,400 km, or +235 km above the GSO orbit; drift 6º/day to west. Satellite finally ceased operation 13 February A TDF1 live television satellite Last orbital position: 19º W. Semi-major axis increased by 300 km. Satellite configured in solar pointing mode and ceased operation in September A TDF2 live television satellite Last orbital position: 36º E. Semi-major axis 42,440 km; drift 3.9º to west. Satellite ceased operation on 1 June B EUTELSAT II F1 telecommunications satellite
9 Registration number Satellite E SARA experimental microsatellite A TC 2A telecommunications satellite Satellite was completely passivated and reorbited about 300 km above the GSO orbit in November 2005 and finally ceased operation A TC 2B telecommunications satellite Satellite was reorbited 188 km above the GSO orbit from orbital position 47º E and finally ceased operation on 23 June C S80T technological satellite A SPOT 3 Earth observation satellite B Stella scientific satellite B ARSENE amateur radio satellite B Cerise space-object technique and technology research satellite A Helios 1B space-object technique and technology research satellite Following a breakdown of its supply system, the satellite was withdrawn from its orbit on 21 October In conformity with IADC recommendations, deorbiting manoeuvres were effected with a view to maximum restriction of the satellite s life in Earth orbit B Idefix amateur radio satellite 9
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