Attachment UN Registration

This document pretains to SAT-MOD-20161003-00096 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2016100300096_1152867

United Nations ST/SG/SER.E/767 Secretariat Distr.: General 16 August 2016 English Original: Spanish 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 15 June 2016 from the Permanent Mission of Mexico to the United Nations (Vienna) addressed to the Secretary-General The Permanent Mission of Mexico to the United Nations (Vienna), 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 transmit information on Mexican satellite E117WB (SATMEX 9) (see annex). V.16-05140 (E) 220816 230816 *1605140*

ST/SG/SER.E/767 Annex Registration data on a space object launched by Mexico* E117WB (SATMEX 9, Eutelsat 117 West B) Information provided in conformity with the Convention on Registration of Objects Launched into Outer Space Name of object launched: E117WB (SATMEX 9, Eutelsat 117 West B) Name of launching State: Mexico Other launching States: United States of America Date of launch: 14 June 2016 Territory or location of launch: Cape Canaveral Air Force Station, Florida, United States of America Basic orbital characteristics Geostationary orbit location: 117 degrees West Inclination: ± 0.05 degrees Longitudinal tolerance: ± 0.05 degrees General function of space object: Communications satellite Date of decay/re-entry/deorbit: 20 December 2031 (expected date) Additional voluntary information for use in the Register of Objects Launched into Outer Space Space object owner or operator: Satélites Mexicanos, S.A. de C.V. (Eutelsat Americas) Launch vehicle: Falcon-9 v1.1 Website: www.spacex.com Technical details for E117WB Orbital position: 117 degrees West Number of transponders: 2 L-band 2 extended C-band 48 extended Ku-band (36 MHz) Date of launch: 14 June 2016 Entry into service: March 2017 Estimated useful life: 15 years Type: Communications satellite __________________ * The registration data are reproduced in the form in which they were received. 2 V.16-05140

ST/SG/SER.E/767 Satellite platform: 702SP (Small Platform) Entry into service: March 2017 Dimensions of satellite Length: 32.6 metres Width: 8.3 metres Height: 4.8 metres Deployed area of solar arrays: 51.7 square metres Type of orbit: Geostationary Orbit altitude: 36,000 kilometres Stabilization mode: Triaxial Precision maintenance: East/West ± 0.05 degrees North/South ± 0.05 degrees Precision of antenna positioning: Antenna pointing ≤ 0.1 degrees Weight of satellite: 2,221.5 kilograms Launch vehicle: Falcon-9 v1.1 Transponders Frequency band Bandwidth per transponder Bandwidth L-band (Wide Area 1166.20-1186.70 MHz (L5) 20 MHz Augmentation System) 1565.17-1586.70 MHz (L1) Extended C-band 3400-3700 MHz (space-Earth) 300 MHz 6425-6725 MHz (Earth-space) Extended Ku-band 10.95-11.20 GHz (space-Earth) 500 MHz 11.45-11.70 GHz (space-Earth) 13.75-14.00 GHz (Earth-space) 14.50-14.80 GHz (Earth-space) V.16-05140 3


Document Created: 2016-10-03 17:33:01
Document Modified: 2016-10-03 17:33:01
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