Globalstar sagedustaotluse ICAO kooskõlastus

Fencing Antenna 1 58.14861 N 24.92194 E Antenna 2 Equipment Shelter 58.14833 N 24.9225 E Antenna 3 58.14778 N 24.92222 E Sagedusloa taotlus kosmoseside maajaamale Application form for Satellite earth station licences 1 Taotleja andmed/ Customer Information Taotleja nimi, isiku- või registrikood/ Applicant and company registration number Globalstar Europe S. A.S Postiaadress/ Postal address 37 rue des Mathurins 75008 Paris France Telefon/ Telephone +1(985) 335-1500 Telefax +1(985) 335-1900 E-Mail [email protected] Aadress / Billing address (if different from postal address) 1351 Holiday Square Boulevard Covington, Louisiana 70433 USA Esindaja nimi/ Name of contact person (responsible for operation) Travis Bennett Postiaadress/ Postal address 1351 Holiday Square Boulevard Covington, Louisiana 70433 USA Telefon/ Telephone +1(985) 335-1585 Telefax +1(985) 335-1900 E-Mail [email protected] Teenuse kasutusinformatsioon / Information regarding the service Teenuse kirjeldus / Type of service (e.g. data/video/audio/telephone) Mobile Satellite Service Eeldatav kasutamise alguse aeg ja soovitav sagedusloa kehtivustähtaeg/ Date of start and end of service TBD- No end date. Maajaam/ Earth station , (for Hub station/additional station(s) copy this sheet and complete this section accordingly) Antenni asukoha aadress/ Address of location 2 ) (samuti maajaam/ antenni asu koht: nt vana/uus mast, millisel hoonel, auto katusel / ALSO description of antenna site: eg. Old/new tower, on wich building, on the top of wich vehicle) Levalohu , Kilingi-Nõmme , Saarde municipality , Pärnu count y, Estonia Antenni a sukoha koordinaadid/ Geographical coordinates 3) Pikkuskraad/ Longitude Laiuskraad/ Latitude Kraadid/ Degrees E/W Minutid/ Minutes Sekundid/ Seconds Kraadid/ Degrees N/S Minutid/ Minutes Sekundid/ Seconds 24 E 55 18.984 58 N 8 54.996 Tootja/ Seadme tüüp/ Manufacturer/Type of equipment/Type approval mark Cobham SATCOM/Antenna Seerianumber/ Serial number Tracker T6000 Saatesagedus/ Sagedus ala / Transmitting Frequency / Frequency band 4) Alumine sageduspiir / Lower limit: 5091 MHz Ülemine sagedus piir / Upper limit : 5250 MHz Vastuvõtusagedus/ Sagedusriba / Receiving Frequency / Frequency band 4) Alumine sagedus piir / Lower limit 6875 MHz Ülemine sagedus piir / Upper limit : 7055 MHz Antenni kõrgus merepinnast/ Antenna altitude from sea level 5) 63.69 m Antenni läbimõõt/ Antenna diameter 6 m Polarisatsioon/ Polarisation 6 ) Left and Right Circular ( CL,CR ) Antenni võimendustegur (saatja) Maximum antenna gain (transmitter) 47.5 dBi Antenni võimendustegur (vastuvõtja) Maximum antenna gain (receiver) 51.2 dBi Kiirgusdiagramm Radiation pattern 7) (give reference pattern or provide diagram) ITU-R S.465 Antenni kiirelaius Antenna beamwidth 8) 0.6 ° Andmeedastuskiirus Data rate of Transmission 20 Kbit/s Vastuvõtja müratemperatuur Receiving system noise temperature 9) 141 °K Kiirgusklass / Designation of emission 10) Tx - 1M23G7W, 4M50G7D , 40K0G2D , 76K0F2D Rx - 1M23G7W, 200KG7D , 70K0G7D , 7K00G1D Väljund võimsus / Total peak power 11) 24.7 dbW Maksimaalne v õimsustihedus / Maximum power density 12) -39 dbW /Hz Maajaama antenni tõusunurk / Earth Station Antenna Elevation angle 13) 10 - 90 Kasutamise eesmärk / Purpose of use 14) MSS feeder link Globalstar GMPCS satellite communications. Modulatsioon / Modulation 15) BPSK/QPSK Satelliit/ Satellite Nimi/ Name Globalstar ITU Constellation : HIBELO-4 , HIBLEO-X Asukoht/ Location (Orbital long. / Deg east) 1414km altitude, 52 degree inclination, Orbit period = 114 minutes 8 orbital planes with 6 spacecraft each, Spacecraft phasing = 7.5 degrees RAAN 0, 45, 90, 135, 180, 225, 270, 315 degrees Saate kiir / Transmitting beam 16) To Earth Station: C Band 6875-7055 MHz Vastuvõt u kiir / Receiving beam 17) From Earth Station: C Band 5091-5250 MHz Kinnitan raadiosidele esitavate nõu ete tundmist ja nende vastavust. I confirm being familiar with the requirements for radiocommunication and compliance therewith. Allkiri/ Signature 18) Allkirjastamise k oht ja aeg/ Place and date Nimi/ Name ( Trükitähtedega / Block letters) 1) Low power VSAT earth stations that operate at 14.0 - 14.25 GHz and that fulfill the requirements in ERC/ DEC( 00)05 are exempted from licensing. 2) For a transportable earth station, give the geographical area where the station will be used. Area should be limited to the actual area needed: street address, part of town, town, county or the whole country. Antenna location may be for example: on ground, on roof, at mast, on trailer, or at roof of a car. 3) Geographical Coordinates The geographical position of the physical centre of the Earth Station Antenna . If the coordination area of the Earth Station Antenna overlaps the territory of another Administration , the precision required is to six seconds. Format: Long/Lat in degrees, minutes and seconds. 4) If more than one carrier will be used, give them in an annex. If only one carrier will be used, but it may be located in a broader range, give here the lowest and highest frequency. 5) Antenna altitude from sea level is measured to the center of the antenna. 6) Polarization : The code for representing the angular relationship between the plane of the electric field vector and the equatorial plane. The angular relationship is observed counter-clockwise in any fixed plane normal to the Beam axis, from the equatorial plane to the electric field vector of the waves, as seen from the satellite. Format: Up to 2 characters. Code Meaning CL Left hand circular or indirect: the electric field vector rotates anti-clockwise. CR Right hand circular or direct: the electric field vector rotates clockwise. D Dual: when substantially equal-amplitude vertically and horizontally polarized components are radiated with-out particular control of the phase relation between them. Typically, the vertically and horizontally polarized sources may be displaced one from the other so that the resultant polarization varies between circular and slant, according to azimuth angle. H Horizontal linear: the electric field vector is in a plane parallel to the equatorial plane. L Linear: the electric field vector remains in the direction specified by the Polarization Linear Angle* . M Mixed: the collective term applied when both vertical and horizontal components are radiated, embracing slant, circular and dual polarization. SL Left hand slant: the electric field vector is in the plane rotated 45 degrees anti-clockwise from the vertical plane. SR Right hand slant: the electric field vector is in the plane rotated 45 degrees clockwise from the vertical plane. V Vertical linear: the electric field vector is in the plane normal to the equatorial plane. * Polarization Linear Angle The angle measured in an anti-clockwise direction, in a plane normal to the beam axis, between the direction of the electric field and a line parallel to the equatorial plane as seen from the satellite. Format: Integer (in the range 0 to 359) in degrees. 7) Antenna radiation pattern may be: - Rec ITU-R 465 - Rec ITU-R 580 - A - B*log(phi) give coefficients A and B A Gain Pattern Equation if the gain pattern can be described by the set of following expressions. G = Gmax for PHI<1 G = a - b * LOG 10 (PHI) for 1 PHI phi1 G = MAX (MIN (G(phi1), c-d* LOG 10 (PHI)), -10) for PHI >phi1 - given in annex 8) Antenna Beamwidth The angular width of the main lobe of radiation, measured in the plane containing the direction of the Maximum Gain, within which the off-axis gain does not fall more than 3 dB below the value of the Maximum Gain . Format: Decimal (in the range 0.00 to 10.00) to 2 decimal places in degrees. 9) Receiving System Noise Temperature The noise temperature is the lowest total value arising from the antenna’s environment, the receiving antenna AND from within the receiving system . For radio waves the Earth is considered to be a “grey” body and for an Associated Earth Station Antenna the sidelobe performance and elevation angle may both be significant factors in the level of environmental noise (ITU-R Satellite Communications Handbook). For Associated Earth Station Antennas the Receiving System Noise Temperature is determined under clear sky conditions and at the Associated Earth Station Antenna’s Planned Minimum Elevation Angle, excluding tolerances for geostationary satellite operation. Format: Integer (in the range 20 to 6000) in Kelvins. 10) See description below in ANNEX1 11) This is the power fed to the antenna. 12) Give the power calculated to a 1 Hz band at the point in spectrum where there is highest level in 4 kHz band for analogue and in 1 MHz band for digital modulation. 13) Enter the planned minimum operating angle of elevation of the antenna in the direction of maximum radiation towards the associated space station, expressed in decimal degrees from the horizontal plane . In the case of a geostationary-satellite network, these angles are to be calculated for the nominal orbital longitude, taking into account the tolerances. 14) Purpose of use may be for example: - TV-transmission - SNG - VSAT - MSS feeder link - BSS feeder link 15) Modulation can be analogue (e.g. FM, PM) or digital (e.g. PSK, QAM or other multilevel phase modulations). 16) Use the ITU (BR) nomenclature. 17) Use the ITU (BR) nomenclature. 18) Signature of applicant or representative of applicant ANNEX 1 Section I. Necessary Bandwidth (1) The necessary bandwidth, as defined in No. S1.152 and determined in accordance with the formulae and examples, shall be expressed by three numerals and one letter . The letter occupies the position of the decimal point and represents the unit of bandwidth. The first character shall be neither zero nor K, M or G. (2) Necessary bandwidths 1 : between 0.001 and 999 Hz shall be expressed in Hz (letter H); between 1.00 and 999 kHz shall be expressed in kHz (letter K); between 1.00 and 999 MHz shall be expressed in MHz (letter M); between 1.00 and 999 GHz shall be expressed in GHz (letter G). (3) For the full designation of an emission, the necessary bandwidth, indicated in four characters, shall be added just before the classification symbols. When used, the necessary bandwidth shall be determined by one of the following methods: (3.1) use of the formulae and examples of necessary bandwidths and designation of corresponding emissions given in Recommendation ITU-R SM.1138; (3.2) computation, in accordance with other ITU-R Recommendations; (3.3) measurement, in cases not covered by (3.1) or (3.2) above. 1 Examples: 0.002 Hz = H002 6 kHz = 6K00 1.25 MHz = 1M25 0.1 Hz = H100 12.5 kHz = 12K5 2 MHz = 2M00 25.3 Hz = 25H3 180.4 kHz = 180K 10 MHz = 10M0 400 Hz = 400H 180.5 kHz = 181K 202 MHz = 202M 2.4 kHz = 2K40 180.7 kHz = 181K 5.65 GHz = 5G65 Designation of emission Basic Characteristics (1) First symbol – type of modulation of the main carrier (1.1) Emission of an unmodulated carrier N (1.2) Emission in which the main carrier is amplitude-modulated (including cases where sub-carriers are angle-modulated) (1.2.1) Double-sideband A (1.2.2) Single-sideband, full carrier H (1.2.3) Single-sideband, reduced or variable level carrier R (1.2.4) Single-sideband, suppressed carrier J (1.2.5) Independent sidebands B (1.2.6) Vestigial sideband C (1.3) Emission in which the main carrier is angle-modulated (1.3.1) Frequency modulation F (1.3.2) Phase modulation G (1.4) Emission in which the main carrier is amplitude- and angle-modulated either simultaneously or in a pre-established sequence D Emission of pulses 1 [ 1 Emissions where the main carrier is directly modulated by a signal which has been coded into quantized form (e.g. pulse code modulation) should be designated under (1.2) or (1.3).] (1.5.1) Sequence of unmodulated pulses P (1.5.2) A sequence of pulses (1.5.2.1) modulated in amplitude K (1.5.2.2) modulated in width/duration L (1.5.2.3) modulated in position/phase M (1.5.2.4) in which the carrier is angle-modulated during the angle-period of the pulse Q (1.5.2.5) which is a combination of the foregoing or is produced by other means V (1.6) Cases not covered above, in which an emission consists of the main carrier modulated, either simultaneously or in a pre-established sequence, in a combination of two or more of the following modes: amplitude, angle, pulse W (1.7) Cases not otherwise covered X (2) Second symbol – nature of signal(s) modulating the main carrier (2.1) No modulating signal 0 A single channel containing quantized or digital information without the use of a modulating sub-carrier 2 ( 2 This excludes time-division multiplex.) 1 (2.3) A single channel containing quantized or digital information with the use of a modulating sub-carrier 1 2 (2.4) A single channel containing analogue information 3 (2.5) Two or more channels containing quantized or digital information 7 (2.6) Two or more channels containing analogue information 8 (2.7) Composite system with one or more channels containing quantized or digital information, together with one or more channels containing analogue information 9 (2.8) Cases not otherwise covered X Third symbol - type of information to be transmitted 3 ( 3 In this context the word “information” does not include information of a constant, unvarying nature such as is provided by standard frequency emissions, continuous wave and pulse radars, etc.) (3.1) No information transmitted N (3.2) Telegraphy – for aural reception A (3.3) Telegraphy – for automatic reception B (3.4) Facsimile C (3.5) Data transmission, telemetry, telecommand D (3.6) Telephony (including sound broadcasting) E (3.7) Television (video) F (3.8) Combination of the above W (3.9) Cases not otherwise covered X Sub-Section IIB. Optional Characteristics for the Classification of Emissions Two optional characteristics should be added for a more complete description of an emission. These are (see also Recommendation 62 ): Fourth symbol – Details of signal(s) Fifth symbol – Nature of multiplexing Where the fourth or fifth symbol is used it shall be as indicated below. Where the fourth or the fifth symbol is not used this should be indicated by a dash where each symbol would otherwise appear. (1) Fourth symbol – Details of signal(s) (1.1) Two-condition code with elements of differing numbers and/or durations A (1.2) Two-condition code with elements of the same number and duration without error-correction B (1.3) Two-condition code with elements of the same number and duration with error-correction C (1.4) Four-condition code in which each condition represents a signal element (or one or more bits) D (1.5) Multi-condition code in which each condition represents a signal element (of one or more bits) E (1.6) Multi-condition code in which each condition or combination of conditions represents a character F (1.7) Sound of broadcasting quality (monophonic) G (1.8) Sound of broadcasting quality (stereophonic or quadraphonic) H (1.9) Sound of commercial quality (excluding categories given in sub paragraphs 1.10 and 1.11) J (1.10) Sound of commercial quality with the use of frequency inversion or band splitting K (1.11) Sound of commercial quality with separate frequency-modulated signals to control the level of demodulated signal L (1.12) Monochrome M (1.13) Colour N (1.14) Combination of the above W (1.15) Cases not otherwise covered X (2) Fifth symbol – Nature of multiplexing (2.1) None N Code-division multiplex 4 ( 4 This includes bandwidth expansion techniques.) C (2.3) Frequency-division multiplex F (2.4) Time-division multiplex T (2.5) Combination of frequency-division multiplex and time-division multiplex W (2.6) Other types of multiplexing X Ardo Oras ICAO sageduste koordinaator Eestis [email protected] Tallinn Meie 29.10.2020 nr 17-1/2020/2166 Globalstar sagedustaotluse ICAO kooskõlastus Austatud Ardo Oras Käesolevaga küsib TTJA kooskõlastust Globalstar Europe S.A.S NGSO satelliitvõrgu maajaamale sagedusloa väljastamiseks Eesti Vabariigi territooriumil. 27.20.2020 laekus TTJA-le ametlik taotlus Globalstar Europe S.A.S poolt sagedusressursi eraldamiseks planeeritava NGSO satelliitvõrgu maajaama rajamiseks. Küsitud saatesageduste vahemik suunal maa-kosmos on 5091-5250 MHz. Vastavalt ESS § 13 lg. 3 vajab nimetatud sagedusvahemik kooskõlastamist ICAO sageduste koordinaatoriga Eestis kuna on osaliselt reserveeritud esmase kasutusõigusega lennunduse MLS maandumissüsteemidele. Planeeritava maajaama asukoht on Levalohu, Kilingi-Nõmme, Saarde vald, Pärnu maakond (24E5518984, 58N0854996). Kasutatav antennisüsteem koosneb kolmest 6m läbimõõduga paraboolantennist võimendusteguriga 47,5 dBi, maksimaalne kasutatav väljundvõimsus 24,7 dBW, maksimaalne võimsustihedus -39dBW/Hz. Maajaama antenni minimaalne tõusunurk on 10 kraadi üle horisondi. Suunal kosmos-maa on küsitud vastuvõtusageduste vahemik 6875-7055MHz, mis on kooskõlas Eesti sagedusplaaniga. Lugupidamisega (allkirjastatud digitaalselt) Erko Kulu Talituse juhataja Lisad: 1. Sagedusloa taotlus 2. Kinnistu asukohaplaan Endla 10a / 10122 Tallinn / tel 667 2000 / faks 667 2001 / [email protected] / www.ttja.ee Registrikood 70003218 Veikko Tunnel 667 2123 [email protected] 2 (2)