NTIA satellite and GS parameters

1288-EX-ST-2015 Text Documents

Cornell University

2016-01-21ELS_171825

Our	
  Spectrum	
  Coordination	
  Branch	
  requires	
  the	
  following	
  additional	
  information	
  for	
  satellite	
  
applications	
  that	
  are	
  not	
  STAs.	
  	
  Please	
  review	
  the	
  information	
  below	
  and	
  submit	
  an	
  exhibit	
  that	
  contains	
  
the	
  data.	
  	
  Reference	
  to	
  the	
  specific	
  data	
  descriptions	
  can	
  be	
  found	
  by	
  Googling	
  the	
  NTIA	
  Red	
  Book	
  under	
  
Chapter	
  9.	
  

PLEASE	
  SUBMIT	
  THE	
  FOLLOWING	
  INFORMATION:	
  

1.)	
  THE	
  TYPE	
  OF	
  SATELLITE,	
  GEOSTATIONARY	
  OR	
  NONGEOSTATIONARY,	
  (XAL	
  AND/OR	
  RAL).	
  

A.)	
  IF	
  ANY	
  SATELLITES	
  ARE	
  GEOSTATIONARY,	
  REPORT	
  ITS	
  LATITUDE	
  AS	
  000000N	
  (XLA	
  AND/OR	
  

RLA)	
  AND	
  REPORT	
  ITS	
  LONGITUDE	
  (XLG	
  AND/OR	
  RLG).	
  

B.)	
  IF	
  ANY	
  SATELLITES	
  ARE	
  NONGEOSTATIONARY,	
  REPORT	
  ITS	
  INCLINATION	
  ANGLE,	
  APOGEE	
  

IN	
  KILOMETERS,	
  PERIGEE	
  IN	
  KILOMETERS,	
  ORBITAL	
  PERIOD	
  IN	
  HOURS	
  AND	
  FRACTIONS	
  OF	
  

HOURS	
  IN	
  DECIMAL,	
  THE	
  NUMBER	
  OF	
  SATELLITES	
  IN	
  THE	
  SYSTEM,	
  THEN	
  T01,	
  EXAMPLE,	
  

REM04	
  *ORB,98.0IN00510AP00510PE001.58H01NRT01,	
  AND	
  FOR	
  SPACE-­‐TO-­‐SPACE	
  

COMMUNICATIONS	
  WITH	
  ANOTHER	
  NONGEOSTATIONARY	
  SATELLITE	
  ADD	
  AN	
  ADDITIONAL	
  

*ORB	
  FOR	
  IT	
  ENDING	
  IN	
  R01,	
  EXAMPLE,	
  REM05	
  *ORB,72.9IN03209AP00655PE013.46H01NRR01	
  

2.)	
  THE	
  SATELLITE	
  TRANSMITTER	
  ANTENNA	
  GAIN	
  AND	
  BEAMWIDTH	
  (XAD),	
  EXAMPLE,	
  XAD01	
  

16G030B	
  

3.)	
  THE	
  SATELLITE	
  TRANSMITTER	
  ANTENNA	
  AZIMUTH	
  (XAZ),	
  NARROWBEAM,	
  NB,	
  EARTH	
  

COVERAGE,	
  EC,	
  EXAMPLE,	
  XAZ01	
  EC	
  OR	
  LEAVE	
  BLANK	
  FOR	
  SPACE-­‐TO-­‐SPACE	
  OPERATIONS.	
  

4.)	
  THE	
  EARTH	
  STATION	
  RECEIVER	
  ANTENNA	
  GAIN,	
  BEAMWIDTH,	
  AZIMUTHAL	
  RANGE,	
  THE	
  SITE	
  

ELEVATION	
  ABOVE	
  MEAN	
  SEA	
  LEVEL	
  IN	
  METERS	
  AND	
  THE	
  ANTENNA	
  HEIGHT	
  ABOVE	
  TERRAIN	
  

IN	
  METERS	
  (RAD),	
  EXAMPLE	
  ASSUMING	
  NONGEOSTATIONARY,	
  RAD01	
  

16G030B000-­‐360A00357H006	
  

5.)	
  THE	
  EARTH	
  STATION	
  RECEIVER	
  ANTENNA	
  AZIMUTH	
  (RAZ),	
  THE	
  MINIMUM	
  ANGLE	
  OF	
  

ELEVATION,	
  V00	
  TO	
  V90,	
  EXAMPLE,	
  RAZ01	
  V00	
  

6.)	
  For	
  Cubesat	
  or	
  Nanosat	
  satellites	
  use	
  S945.	
  	
  The	
  reference	
  name	
  shall	
  be	
  added	
  in	
  the	
  circuit	
  remarks	
  	
  

THE	
  S	
  NOTE	
  (ASSUMING	
  NONGEOSTATIONARY,	
  USE	
  S945-­‐-­‐THIS	
  ASSIGNMENT	
  SUPPORTS	
  

OF	
  THE	
  NON-­‐GEOSTATIONARY	
  CUBESAT	
  TEST	
  BED	
  (CSTB)	
  SATELLITE).	
  

7.)	
  THE	
  TRANSMITTER	
  ANTENNA	
  ORIENTATION	
  (XAP),	
  EXAMPLE	
  XAP01	
  J	
  ,	
  AND	
  THE	
  RECEIVER	
  

ANTENNA	
  ORIENTATION	
  (RAP),	
  EXAMPLE	
  RAP01	
  J	
  ,	
  WHERE	
  J	
  REPRESENTS	
  LINEAR	
  


POLARIZATION.	
  OTHER	
  POLARIZATIONS	
  INCLUDE	
  H	
  FOR	
  HORIZONTAL,	
  V	
  FOR	
  VERTICAL,	
  S	
  

FOR	
  HORIZONTAL	
  AND	
  VERTICAL,	
  L	
  FOR	
  LEFT	
  HAND	
  CIRCULAR,	
  R	
  FOR	
  RIGHT	
  HAND	
  

CIRCULAR,	
  T	
  FOR	
  RIGHT	
  AND	
  LEFT	
  HAND	
  CIRCULAR,	
  E	
  FOR	
  ELLIPTICAL	
  AND	
  O	
  FOR	
  OBLIQUE	
  

ANGLED	
  CROSSED.	
  

	
  

REM01	
  *ORB,51.6IN00410AP00400PE001.50H01NRT01	
  

XAD01	
  01G091B	
  

XAZ01	
  EC	
  

RAD01	
  17G030B000-­‐360A00280H006	
  

RAZ01	
  V00	
  

*AGN,	
  Cubesat,	
  KickSat-­‐2	
  

XAP01	
  J	
  

RAP01	
  R	
  



Document Created: 0250-04-24 00:00:00
Document Modified: 0250-04-24 00:00:00

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