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IBFS / ICFS

SES-AMD-20040817-01198

Telesat

Proposed transportable earth station will be capable of simulating a Ka-band Hub and/or Ka-band remote primarily for troubleshooting, testing, etc., should any payload performance issues come up on any of the US KA gateways or user beams.

Filing overview

StatusAction Taken Public Notice
Call signE040285
Contact|TELESAT CANADA|1601 Telesat Court, Gloucester|Ontario, Canada K1B5P4|CANADA K1B 5P4, - CAN |
Date filed2004-08-11
Status date2004-09-22
Grant date2004-09-21
ServiceDomestic Fixed Satellite ServiceFixed Satellite ServiceInternational Fixed Satellite Service
Last actionGrant of Authority

Frequencies

Lower MHzUpper MHzEmissionLocation
18300.00000018800.000000
19700.00000020200.000000
28350.00000028600.000000
29250.00000029500.000000
29500.00000030000.000000

Sites

SiteAddressCoordinatesDatum
F2KA Transportable  ,  ,  ,           NA

Antennas

AntennaManufacturerModelDiameter (m)QuantityDetails
F2KAANDREWESA24SNG-LTE2.4001<TABLE BORDER=2 WIDTH="100%"><TR><TD><TABLE BORDER=0 WIDTH="100%"><TR><TD >Site ID: F2KA Transportable</TD><TD >Antenna ID: F2KA <TR><TD >Manufacturer: ANDREW</TD><TD >Diameter (meters): 2.4<TR><TD >Model: ESA24SNG-LTE</TD><TD >Diameter Minor (m): 0<TR><TD >Building Height AGL (m): 2.4</TD><TD >Diameter Major (m): 0<TR><TD >Max Antenna Height AGL (m): 5.4</TD><TD >Quantity: 1<TR><TD >Max Antenna Height AMSL (m): </TD><TD >Total Power (Watts): 14.35<TR><TD >Max Antenna Height Above Rooftop (m): 3</TD><TD >Total EIRP (dBW): 66.7</TABLE></TD></TR></TABLE><TABLE ><TR ><TH >Antenna Gain (dBi)</TH><TH >@ (Ghz)</TH></TR><TR><TD>51.7</TD><TD>19</TD></TR><TR><TD>55.13</TD><TD>29</TD></TR></TABLE><TABLE ><TR ><TH >Polarization</TH><TH >Max EIRP/Carrier (dBW)</TH><TH >Max EIRP Density/Carrier (dBW)</TH><TH >Emission Designator</TH><TH >Frequency Lower (MHz)</TH><TH >Frequency Upper (MHz)</TH><TH >T/R Mode</TH></TR><TR><TD>R</TD><TD>&nbsp;</TD><TD>&nbsp;</TD><TD>1M60G7W</TD><TD>18300.0000</TD><TD>18800.0000</TD><TD>R</TD></TR><TR><TD>L</TD><TD>&nbsp;</TD><TD>&nbsp;</TD><TD>25M2G7W</TD><TD>19700.0000</TD><TD>20200.0000</TD><TD>R</TD></TR><TR><TD>L</TD><TD>66.7</TD><TD>29.5</TD><TD>25M2G7W</TD><TD>28350.0000</TD><TD>28600.0000</TD><TD>T</TD></TR><TR><TD>L</TD><TD>66.7</TD><TD>29.5</TD><TD>25M2G7W</TD><TD>29250.0000</TD><TD>29500.0000</TD><TD>T</TD></TR><TR><TD>R</TD><TD>50.24</TD><TD>25.19</TD><TD>1M60G7W</TD><TD>29500.0000</TD><TD>30000.0000</TD><TD>T</TD></TR></TABLE><TABLE ><TR ><TH >Azimuth Angle Eastern Limit</TH><TH >Azimuth Angle Western Limit</TH><TH >Antenna Elevation Angle Eastern Limit</TH><TH >Antenna Elevation Angle Western Limit</TH><TH >Lower Fre- quency Limit</TH><TH >Upper Fre- quency Limit</TH><TH >Max EIRP Density (dBW/ 4KHz)</TH><TH >Satellite Arc Eastern Limit</TH><TH >Satellite Arc Western Limit</TH><TH >Satellite Orbit Type</TH></TR><TR><TD>0</TD><TD>0</TD><TD>34.4</TD><TD>15.1</TD><TD>18300.0000</TD><TD>18800.0000</TD><TD>&nbsp;</TD><TD>62 W</TD><TD>144 W</TD><TD>G</TD></TR><TR><TD>0</TD><TD>0</TD><TD>34.4</TD><TD>15.1</TD><TD>19700.0000</TD><TD>20200.0000</TD><TD>&nbsp;</TD><TD>62 W</TD><TD>144 W</TD><TD>G</TD></TR><TR><TD>0</TD><TD>0</TD><TD>34.4</TD><TD>15.1</TD><TD>28350.0000</TD><TD>28600.0000</TD><TD>-26.1</TD><TD>62 W</TD><TD>144 W</TD><TD>G</TD></TR><TR><TD>0</TD><TD>0</TD><TD>34.4</TD><TD>15.1</TD><TD>29250.0000</TD><TD>29500.0000</TD><TD>-26.1</TD><TD>62 W</TD><TD>144 W</TD><TD>G</TD></TR><TR><TD>0</TD><TD>0</TD><TD>34.4</TD><TD>15.1</TD><TD>29500.0000</TD><TD>30000.0000</TD><TD>-30.4</TD><TD>62 W</TD><TD>144 W</TD><TD>G</TD></TR></TABLE>

Public notices

DateReportTypeServiceStatus
2004-09-22SES00643 Action Taken Public NoticeSatellite Earth Station0

Sources and provenance

SourceSource recordRetrievedMatch
ICFSSES-AMD-20040817-011982026-07-30 08:55:12Source Primary
Selected field provenance
FieldDisplayed valueSourceObserved
StatusAction Taken Public NoticeICFS SES-AMD-20040817-011982026-07-30 08:55:12
DescriptionProposed transportable earth station will be capable of simulating a Ka-band Hub and/or Ka-band remote primarily for troubleshooting, testing, etc., should any payload performance issues come up on any of the US KA gateways or user beams.ICFS SES-AMD-20040817-011982026-07-30 08:55:12
Applicant NameTelesatICFS SES-AMD-20040817-011982026-07-30 08:55:12
Call SignE040285ICFS SES-AMD-20040817-011982026-07-30 08:55:12
Date Filed2004-08-11ICFS SES-AMD-20040817-011982026-07-30 08:55:12
Status Date2004-09-22ICFS SES-AMD-20040817-011982026-07-30 08:55:12
Grant Date2004-09-21ICFS SES-AMD-20040817-011982026-07-30 08:55:12
Expiration Date0000-00-00ICFS SES-AMD-20040817-011982026-07-30 08:55:12

Documents

DocumentTypeDateStatus
Attachment Exhibit 42a Invalid document
Attachment Application Available
Attachment HTML Invalid document