Examples

• Here's an overview of current ring intel.
  (هذا ملخص لمعلومات عن (رينج
• The Ring product list is currently being developed by the Global Office.
  والمكتب العالمي عاكف حاليا على إعداد هذه القائمة.
• The model is adjusted using the energy balance equation for the current ring, which takes into account the real Dst values.
  ويضبط النموذج باستخدام معادلة ميزانية الطاقة المتعلقة بحلقة التيار، التي تأخذ في الحسبان القيم الحقيقية لدليل الاضطرابات المغنطيسية الأرضية (Dst).
• Information furnished in conformity with the Convention on Registration of Objects Launched into Outer Space Note verbale dated 7 October 2004 from the Permanent Mission of Germany to the United Nations (Vienna) addressed to the Secretary-General The Permanent Mission of Germany 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 concerning space objects launched by Germany (see annex). Annex Registration data on space objects launched by Germany* Equator-S Register number: D-R012 Type: Unmanned spacecraft Launching State: Germany Designation of space object: Equator-S Date and location of launch: 2 December 1997 Kourou, French Guiana Basic orbital parameters: Period: 22.3 hours Inclination: 4 degrees Apogee: 67,275 kilometres Perigee: 497 kilometres General function: Provides high-resolution plasma, magnetic, and electrical field measurements in the interplanetary region, in particular the low latitude dayside magnetopause and its boundary layer, the equatorial ring current region, and the near-Earth equatorial plasma sheet Date of registration in the Aircraft Register of the Federal Republic of Germany under “Spacecraft”: 16 February 1999 Register number: D-R013 Type: Unmanned spacecraft Launching State: Germany Designation of space object: SAFIR-2 Date and location of launch: 10 July 1998 Baikonur, Kazakhstan Basic orbital parameters: Period: 101 minutes Inclination: 98.8 degrees Apogee: 817 kilometres Perigee: 817 kilometres General function: Satellite for bi-directional data communications at low bit rates Date of registration in the Aircraft Register of the Federal Republic of Germany under “Spacecraft”: 16 February 1999 Register number: D-R020 Type: Unmanned spacecraft Launching State: Germany Designation of space object: DLR-TUBSAT Date and location of launch: 26 May 1999 Sriharikota, India Basic orbital parameters: Period: 99.4 minutes Inclination: 98.38 degrees Apogee: 724 kilometres Perigee: 724 kilometres General function: Experimental satellite for earth observations in the visible spectrum Date of registration in the Aircraft Register of the Federal Republic of Germany under “Spacecraft”: 19 January 2000 AMSAT-Oscar 40 Register number: D-R025 Type: Satellite Launching State: Germany Designation of space object: AMSAT Oscar 40 Date and location of launch: 15 November 2000 Kourou, French Guiana Basic orbital parameters: Period: 1,147 minutes Inclination: 9 degrees Apogee: 59,000 kilometres Perigee: 1,200 kilometres General function: Research and newscast satellite Date of registration in the Aircraft Register of the Federal Republic of Germany under “Spacecraft”: 15 July 2004 Register number: D-R026 Type: Satellite Launching State: Germany Designation of space object: RUBIN 2 Date and location of launch: 20 December 2002 Baikonur, Kazakhstan Basic orbital parameters: Period: Approximately 90 minutes Inclination: 65 degrees Apogee: 650 kilometres Perigee: 650 kilometres General function: Technology experiments and data transfer via the Orbcomm system Date of registration in the Aircraft Register of the Federal Republic of Germany under “Spacecraft”: 6 September 2004
  لجنة استخدام الفضاء الخارجي في الأغراض السلمية معلومات مقدّمة وفقا لاتفاقية تسجيل الأجسام المطلقة في الفضاء الخارجي مذكرة شفوية مؤرخـة 7 تشرين الأول/أكتوبر 2004 موجّهـة إلى الأمين العام من البعثة الدائمة لألمانيا لدى الأمم المتحدة (فيينا) تهدي البعثة الدائمة لألمانيا لدى الأمم المتحدة (فيينا) تحياتها إلى الأمين العام للأمم المتحدة وتتشرف بأن تقدّم، وفقا للمادة الرابعة من اتفاقية تسجيل الأجسام المطلقة في الفضاء الخارجي (مرفق قرار الجمعية العامة 3235 (د-29)) معلومات عن الأجسام الفضائية التي أطلقتها ألمانيا (انظر المرفق). المرفق بيانات التسجيل الخاصة بالأجسام الفضائية التي أطلقتها ألمانيا* Equator-S ـــــــــــــــــــــــــــــــــــــ