A2a
A2b
A2c
A3a
A3b
A4a1
A4a2a
A4a2b
A4b1
A4b3a
A4b3b
A4b4a
A4b4b
A4b4d
A4b4e
A4b4f
A4b5b
A4b5c
A4b6a1
A4b6a2
A4b6a3
A4b6c
A4b6d
A4b6e
A4b6f
A4b6g
A4b6h
A4b6i
A4b6j
A4b7a
A6
A7a1
A7a2
A7a3
A7b1
A7b2
A7c1
A4b7b
A4b7c
A4b7d1
A4b7d2
A4b7d3
A4c1
A4c2
A5
A7c2
A7d
A7e
A7f
Items
A1a
A1b
A1e1
A1e2
A1e3a
A1e3b
A1f1
A1f2
Description
Identity of the satellite network
Plan beam identification
Type of earth station (specific or typical)
Name of the station
Country or geographical area in which the station is located, using the symbols from the Preface
Geographical coordinates of each transmitting or receiving antenna site constituting the station (longitude and latitude in degrees and minutes)
Notifying administration (Refer to Table 1 of the Preface)
If the notice is submitted on behalf of a group of administrations, the symbols of each of the administrations in the group, submitting the information on the satellite network (see the Preface)
Date of bringing into use
Period of validity (years)
Date of bringing into use (radio astronomy station)
Operating agency (Refer to Table 12A/12B of the Preface)
Symbol identifying the Administration responsible for the station (Refer to Table 12A/12B of the Preface)
Nominal longitude of a geostationary space station (degrees)
Planned longitudinal tolerance easterly limit
Planned longitudinal tolerance westerly limit
Number of orbital planes
Maximum number of space stations in a non-geostationary-satellite system simultaneously transmitting on a co-frequency basis in the fixed-satellite service in the Northern Hemisphere
Maximum number of space stations in a non-geostationary-satellite system simultaneously transmitting on a co-frequency basis in the fixed-satellite service in the Southern Hemisphere
Inclination angle for the orbital plane (degrees)
Number of satellites in each orbital plane
Altitude of the apogee (km)
Altitude of the perigee (km)
Minimum altitude of the space station above the surface of the Earth at which any satellite transmits (km)
Initial phase angle (degrees)
Argument of perigee
Maximum number of non-geostationary satellites transmitting with overlapping frequencies to a given location
Associated start of the latitude range (degrees)
Associated end of the latitude range (degrees)
Flag indicating if the space station uses [Y] or does not use [N] station-keeping to maintain a repeating ground track
Time in seconds that it takes for the constellation to return to its starting position
Flag indicating if the space station should [Y] or should not [N] be modelled with specific precession rate of the ascending node of the orbit instead of the J2 term
Precession rate in degrees/day measured counter-clockwise in the equatorial plane
Longitude of the ascending node for the j-th orbital plane
Date at which the satellite is at the location defined by the longitude of the ascending node
Time at which the satellite is at the location defined by the longitude of the ascending node
Longitudinal tolerance of the longitude of the ascending node
Maximum number of non-geostationary satellites receiving simultaneously with overlapping frequencies from the associated earth stations within a given cell
Average number of associated earth stations transmitting with overlapping frequencies per square km in a cell
Average distance between co-frequency cells (km)
Type of zone (based on topocentric angle (Y), satellite-based angle (N) or other method (O) for establishing the exclusion zone)
Width of the exclusion zone (degrees)
Attachment indicating a detailed description of the avoidance mechanism, if an alternative method used for establishing exclusion zone
Associated space station
Nominal orbital longitude
Coordination information, reference to provision of the RR, Appendix or Resolution (Table 11 of the Preface)
Coordination information, reference to provision of the RR, Appendix or Resolution (Table 11 of the Preface)
Horizon elevation angle for each azimuth around the earth station, for each azimuth around the earth station (degrees)
Distance from the earth station to the horizon for each azimuth around the earth station (km)
Horizon elevation diagram
Planned minimum angle of elevation of the antenna’s main beam axis from the horizontal plane (degrees)
Planned maximum angle of elevation of the antenna’s main beam axis from the horizontal plane (degrees)
Start azimuth for the planned range of operating azimuthal angles for the antenna’s main beam axis clockwise from True North (degrees)
End azimuth for the planned range of operating azimuthal angles for the antenna’s main beam axis clockwise from True North (degrees)
Altitude of the antenna above mean sea level (m)
Minimum elevation angle (degrees)
Antenna diameter (m)

Items
A11b
A12
A13
A13c
A13d
A13e
A15a
A16a
A16b
A17a
A17b1
A17b2
A17b3
A17c
A17d
A17e1a
A17e1b
A17e1c
A17e2a
A17e2b
A17e2c
A18a
A19a
B4a3a2
B4b2
B4b3
B4b4a
B4b4b
B4b4c
B4b4d
B4b5
B5a
B3c2a1
B3d
B3e
B3f1
B3f2a
B3f2b
B3f2c
B3f2d
B4a1
B4a2
B1a
B1b
B2bis.a
B2bis.b
B3a1
B3a2
B3b1
B3b2
B3c1a1
B3c1a2
B3c1a3
Description
Stop time UTC
Range of automatic gain control (dB)
Reference to Special Sections
Reference in accordance with Article 4 of Appendix 30
Reference in accordance with Article 4 of Appendix 30A
Reference in accordance with Article 6 of Appendix 30B
Flag to indicate commitment that the filed for system will meet the additional operational epfd limits that are specified in Table 22-4A1 under No. 22.5I.
Flag to indicate commitment that the associated earth stations operating with a geostationary-satellite network in the fixed-satellite service meet the off-axis power limitations
Flag to indicate commitment that the filed system will meet the single entry power-flux density limits specified in No. 5.502
Flag to indicate commitment of compliance with per-satellite power-flux density level produced at the Earth’s surface of
–129 dB(W/m² · MHz) in any 1 MHz band under free space propagation conditions
Calculated aggregate power flux-density produced at the Earth’s surface by any geostationary radionavigation-satellite system in the band 4 990-5 000 MHz in a 10 MHz bandwidth, (Resolution 741 (WRC-03))
Calculated aggregate power flux-density produced at the Earth’s surface by all space stations within any radionavigation-satellite service system in the band 5 030-5 150 MHz in a 150 kHz bandwidth (No. 5.443B)
Equiv. power flux-density produced at the Earth’s surface by all space stations within any non-geostationary radionavigation-satellite service system in the band 4 990-5 000 MHz in a 10 MHz bandwidth, as defined in resolves 2 of Resolution 741 (WRC-03)
Aggregate power flux-density produced at the Earth’s surface in the band 15.35-15.4 GHz, as defined in No. 5.511A
Mean power flux-density produced at the Earth’s surface by any spaceborne sensor, as defined in No. 5.549A
Calculated epfd in the band 42.5-43.5 GHz at RA SDT - dB(W/(m²·/1 GHz))
Calculated epfd in the band 42.5-43.5 GHz at RA SDT - dB(W/(m²·/500 kHz))
Calculated epfd in the band 42.5-43.5 GHz at RA VLBI - dB(W/(m²·/500 kHz))
Calculated pfd in the band 42.5-43.5 GHz at RA SDT - dB(W/(m²·/1 GHz))
Calculated pfd in the band 42.5-43.5 GHz at RA SDT - dB(W/(m²·/500 kHz))
Calculated pfd in the band 42.5-43.5 GHz at RA VLBI - dB(W/(m²·/500 kHz))
Commitment regarding characteristics of aircraft earth station
Commitment that the use of the assignment shall not cause unacceptable interference to, nor claim protection from, those assignments for which agreement still needs to be obtained
Designation of the satellite antenna beam
Flag showing whether the antenna beam, under B.1.a, is fixed or whether it is steerable (reconfigurable) indicator specifying whether the space station only transmits when visible from notified service area
Minimum elevation angle above which transmissions occur when the space station is visible from the notified service area
Maximum co-polar isotropic antenna gain (dBi)
Maximum cross-polar isotropic antenna gain (dBi)
Co-polar antenna gain contours diagram
Cross-polar antenna gain contours diagram
Co-polar reference radiation pattern
Co-polar radiation pattern diagram coefficient A
Co-polar radiation pattern diagram coefficient B
Cross-polar reference radiation pattern
Pointing accuracy (degrees)
Antenna gain vs orbit longitude diagram
Boresight or aim point of the antenna beam (longitude and latitude)
Rotational accuracy (degrees)
Major axis orientation (degrees)
Major axis (degrees)
Minor axis (degrees)
Reference number of each orbital plane in which the space station antenna characteristics are used
Reference number of each satellite, in the specified orbital plane, on which the space station antenna characteristics are used
Beta angle (degrees)
Diagram of the antenna gain as a function of elevation angle
Spreading loss as a function of elevation angle
Maximum E.I.R.P. / 4kHz
Average E.I.R.P. / 4kHz
Maximum E.I.R.P. / 1MHz
Average E.I.R.P. / 1MHz
Calculated peak value of power flux-density produced within ± 5° inclination of the geostationary-satellite orbit
Maximum isotropic gain (dBi)

Items Description
B5c1a6 PHI1
B5d Antenna dimension aligned with the geostationary arc (DGSO) (m)
B6a6 PHI1
C1a
C1b
Lower limit of the frequency range
Upper limit of the frequency range
C8e1
C8e2
C8f1
C8f2
C8g1
C8g2
C8g3
C8h
C8i
C9
C9a1
C9a2a
C9a2b
C9a2c
C9a3a
C7b
C8a1
C8a2
C8b1
C8b2
C8b3a
C8b3b
C8c1
C8c2
C8c3
C8c4
C8d1
C2c
C3a
C3b
C4a
C4b
C5a
C5b
C5c
C5d1
C5d2
C6a
C6b
C9a3c
C9a4b
C9a5a
C9a5b
C9a6a
C9a6b
C9a6c
C9a7
If the frequency assignment is to be filed under No. 4.4, an indication to that effect
Assigned frequency band (kHz)
Bandwidth of the frequency band observed
Class of station (Refer to Table 3 of the Preface)
Nature of service (Refer to Table 4 of the Preface)
Receiving system noise temperature (Kelvin) in the case of a space station
Receiving system noise temperature (Kelvin) in the case of an earth station
Receiving system noise temperature (Kelvin) of a radio astronomy station
System noise temperature at the output of the signal (for active sensors) processor
Receiver noise bandwidth (for active sensors)
Type of polarization (Refer to Table 5 of the Preface)
Polarization angle (degrees) (Refer to Table 5 of the Preface)
Carrier frequency of the emissions
Maximum power supplied to the antenna (dBW)
Maximum power density (dB(W/Hz))
Maximum power supplied to the antenna (dBW)
Maximum power density (dB(W/Hz))
Mean peak envelope power (dBW) supplied to the input of the antenna (required if neither C.8.a.1 nor C.8.b.1 is provided) (for active sensors)
Mean power density (dB(W/Hz)) supplied to the input of the antenna (required if neither C.8.a.2 nor C.8.b.2 is provided) (for active sensors)
Minimum peak power (dBW)
If C.8.c.1 is not provided, the reason for absence of the minimum value of the peak envelope power
Minimum power density (dB(W/Hz))
If C.8.c.3 is not provided, the reason for absence of the minimum power density
Maximum total peak power (dBW)
Carrier-to-noise ratio (dB)
If C.8.e.1 is not provided, the reason for absence of the carrier-to-noise ratio
Space station’s nominal equivalent isotropically radiated power(s) (e.i.r.p.) on the beam axis
Associated space station’s nominal equivalent isotropically radiated power(s) (e.i.r.p.) on the beam axis
Maximum aggregate power (dBW)
The aggregate bandwidth of all carriers (per transponder, if applicable) supplied to the input of the transmitting antenna of the earth station or the associated earth station
Flag indicating if the bandwidth of the transponder corresponds to the aggregate bandwidth of all carriers (per transponder, if applicable) supplied to the input of the transmitting antenna of the earth stations
Maximum power density per Hz supplied to the input of the antenna, in dB(W/Hz), averaged over the necessary bandwidth
Range of power control (dB)
Information on modulation characteristics
Type of modulation
Lowest frequency of the baseband
Highest frequency of the baseband
The r.m.s. frequency deviation of the pre-emphasized signal for a test tone as a function of baseband frequency
Frequency deviation (MHz/V)
Type of multiplexing of the video and sound signals
Number of phases
Nature of the modulating signal
Kind of amplitude modulation used
Peak-to-peak frequency deviation of the energy dispersal waveform (MHz)
Sweep frequency of the energy dispersal waveform (kHz)
Energy dispersal waveform
Type of energy dispersal

Items
C9a8
C10d9
C11a1
C11a2
C11a3
C11a4
C11a5a
C11a5b
C11a5c
C11a5d
C11a5e
C11b
C12a
C13a
C13b
C13c
C15a
C16a1
C16a2
C16b1
C10d5a1a
C10d5a1b
C10d5a1c
C10d5a1d
C10d5a1e
C10d5a1f
C10d5a2
C10d5b1a
C10d5b2
C10d6
C10d7
C10d8
C9b2
C9c1
C9c2
C10a1a
C10a1b
C10a2
C10a3
C10a4a
C10a4b
C10b1
C10b2
C10c1
C10c2
C10d1
C10d2
C10d3
D1a2
D1a3
D2a1
D2a2
D2b1
D2b2
D2c
D2d
2D
11C2
13A
13B1
13B2
13B3
13C
Description
For All other types of modulation, such particulars as may be useful for an interference study
Composition of the baseband
Type of multiple access
Description of the spectrum mask
Identity of the associated space station
Previous identity of the associated space station
Type of associated space station: geostationary [G] or non-geostationary [N]
Nominal longitude of the associated geostationary space station
Designation of the antenna beam of the associated space station
Designation of the old antenna beam of the associated space station
Identity of the associated earth station
Type of associated earth station: specific [S], typical [T] or radioastronomy [R]
Geographical coordinates of the antenna site
Country or geographical area in which the earth station is located, using the symbols from the Preface
Class of station of the associated earth station (Refer to Table 3 of the Preface)
Nature of service of the associated earth station (Refer to Table 4 of the Preface)
Isotropic gain of the antenna (dBi)
Co-polar reference radiation pattern of the associated earth station
Co-polar radiation pattern diagram coefficient A
Co-polar radiation pattern diagram coefficient B
Co-polar radiation pattern diagram coefficient C
Co-polar radiation pattern diagram coefficient D
Co-polar radiation pattern diagram angle
Co-polar radiation pattern diagram of the associated earth station
Cross-polar reference radiation pattern of the associated earth station
Cross-polar radiation pattern diagram of the associated earth station
Receiving system noise temperature (Kelvin) of the associated earth station
Antenna diameter (m)
The equivalent antenna diameter (i.e. the diameter, in metres of a parabolic antenna with the same off-axis performance as the receiving associated earth station antenna)
Associated earth station antenna dimension aligned with the geostationary arc (DGSO) (m)
Service area no. (GIMS)
Service area symbol
Service area diagram attachment
Narrative description of the service area
Service area identified by a set of a maximum of twenty test points
Test point longitude
Test point latitude
Test point altitude
Minimum elevation angle (degrees)
Affected region diagram
Minimum acceptable aggregate carrier-to-interference ratio
Class of observations
Type of radio astronomy station. Single-dish (S) or Very long baseline interferometry (V)
Minimum elevation angle at which the radio astronomy station conducts single-dish or VLBI observations in the frequency band
Description of the group(s) required in the case of non-simultaneous emissions
Pulse length (μs) (for active sensors)
Pulse repetition frequency (kHz) (for active sensors)
Sensitivity threshold (kelvins) (for passive sensors)
Downlink beam designation
Uplink assigned frequency
Lowest equivalent satellite link noise temperature
Associated transmitting gain (lowest)
Satellite link noise temperature for highest ratio of gain/noise
Associated transmitting gain (highest)
Line number for a given set of equivalent satellite link noise temperatures and transmission gain values
Associated receiving earth station name
Date from which an assignment is taken into account according to the RR
Symbols in “agree_st” column of the table “tr_provn” (Table 11C2 of the Preface)
Conformity with Radio Regulations; Table 13A of the Preface
Reference to a provision, appendix or resolution; Table 13B1 of the Preface
Remarks concerning the findings entered in column 13A; Table 13B2 of the Preface
Date relating to the review of the findings. Table 13B3 of the Preface
Remarks (Table 13C of the Preface)

Items Description
BR25
BR26
BR27
BR28
BR30
BR31
BR8
BR9
BR14
BR15
BR16
BR17
BR18
BR4
BR5
BR6a
BR6b
BR6c
BR7a
BR7b
BR19
BR20
BR21
BR22
BR3a
BR3b
Provision reference code
B = Appendix 30 / Appendix 30A
C = Network in coordination stage
N = Network in notification stage
P = Appendix 30B
Fisrt date of bringing into use
Symbol of the geographical area in which the station is located
Identification number of the network
Old identification number of the network
Linked identification number of the network
Identification number of the group
Old identification number of the group
Code indicating the action to be taken on the entity (beam)
Code indicating the action to be taken on the entity (group)
Symbol and number of the Special Section
Provision reference code for the frequency group
Value of type C8b
Old beam designation
Power density [dBW/Hz] averaged over the necessary bandwidth of a narrow bandwidth carrier
Reference to the BR IFIC number published in Part I-S
BR IFIC number
Part of the BR IFIC
Administration remarks (Refer to Table 13C of the Preface)
A = Network in MIFR or for which coordination request has been published
T = Network under examination
C = Network shown in this line causes interference to the network being published
R = Network shown in this line receives interference from the network being published
A = Detected by coordination arc
Name of the spacecraft manufacturer
Date of execution of the contract
BR33
BR34
BR35
BR36
BR37
BR38
BR39
Number of satellites procured
Name of the launch vehicle provider
Name of the launch vehicle
Date of execution of the contract
Anticipated launch or in-orbit "delivery window"
Name of the launch facility
Country / location
BR41 Commercial name of the satellite
BR44 Beamlet
BR45
BR46
Maximum equivalent protection margin degradation (Regions 1 and 3 ) or maximum overall equivalent protection margin degradation
(Region 2)
Maximum power flux density excess
BR62
BR63
BR64
BR65
BR66
BR67
BR68
BR71
BR72
BR73
BR74
BR75
BR52 Part of the IFIC
BR54
BR55
Number of emissions
Number of units
BR56 Total number of units
BR57 Category
BR59 Azimuth
Expiry date for bringing into use
Confirmed date of bringing into use
Date of receipt of 1st Res49
Date of receipt of Part A submission
Date of entry into Plan/List of an allotment/assignment
Expiry date for use of a group of assignments
Date of receipt of launch failure
Expiry date for the period of validity for the frequency assignments
Maximum single-entry C/I degradation (Earth to Space) (dB)
Maximum single-entry C/I degradation (Space to Earth) (dB)
Aggregate C/I degradation (dB)
Total number of units in Part II-S

Items
BR76
BR77
BR78
BR79
BR80
BR81
BR82
BR83
BR84
BR85
BR86
BR87
BR88
BR89
BR90
BR91
BR92
BR94
BR95
Description
Total number of units in Part III-S
Overall number of units in this filing
Date of resumption of operation
Maximum C/I degradation (dB)
‘Allotment’ = allotment in the Appendix 30B Plan.
‘List’ = assignment in the Appendix 30B List
‘Pending’ = pending assignment under coordination before possible inclusion in the List
Date of suspension of use
Date of resumption of use foreseen
Date limit of resumption of use
Priority access date
Unique ITU ID number of the spacecraft
Code indicating regulatory status
F = First bringing into use
S = Suspended
R = Resumed
Date of regulatory status (first bringing into use, suspending or resuming)
Reason for suspension (MOVED, FAILURE, DE-ORBITED or alternative text)
Number of the BR IFIC in which subject Special Section was published
Delivery date of the spacecraft
Launch date of the spacecraft
Number of the attachment for explanation when angle alpha or angle beta cannot be provided
Lower limit of the frequency range on board of the spacecraft
Upper limit of the frequency range on board of the spacecraft