Attachment Sched S Tech Report. SES-STA-20120629-00623

Attachment Sched S Tech Report.

This document pretains to SES-STA-20120629-00623 for Special Temporal Authority on a Satellite Earth Station filing.

IBFS_SESSTA2012062900623_961388

FCC 312 FEDERAL COMMUNICATIONS COMMISSION Page 1: General,
Schedule S SATELLITE SPACE STATION AUTHORIZATIONS Frequency Bands,
(Technical and Operational Description) and GSO Orbit

S1. GENERAL INFORMATION Complete for all satellite applications.
a. Space Station or Satellite Network Name: e. Estimated Date of Placement into Service: i Will the space station(s) operate on a Common Carrier Basis:
EXPRESS AM44 5/19/2009 N

b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis:
3/1/2007 12 Years 0

c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth:
1/1/2009 26 0 MHz

d1. Est Launch Date Begin: d2. Est Launch Date End: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply:
2/11/2009 2/11/2009 1264 MHz GSO NGSO
X

S2. OPERATING FREQUENCY BANDS Identify the frequency range and transmit/receive mode for all frequency bands in which this station will oper
Also indicate the nature of service(s) for each frequency band.
Frequency Band Limits f.
Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode Nature of Service(s): List all that apply to this band
a. Numeric b. Unit c. Numeric d. Unit
(K/M/G) (K/M/G)
3655 M 3695 M T Fixed Satellite Service
5980 M 6020 M R Fixed Satellite Service
3705 M 3745 M T Fixed Satellite Service
6030 M 6070 M R Fixed Satellite Service
3755 M 3795 M T Fixed Satellite Service
3805 M 3845 M T Fixed Satellite Service
6130 M 6170 M R Fixed Satellite Service
3855 M 3895 M T Fixed Satellite Service
6180 M 6220 M R Fixed Satellite Service
3905 M 3945 M T Fixed Satellite Service
6230 M 6270 M R Fixed Satellite Service
4005 M 4045 M T Fixed Satellite Service
6330 M 6370 M R Fixed Satellite Service
4055 M 4095 M T Fixed Satellite Service
6380 M 6420 M R Fixed Satellite Service
4105 M 4155 M T Fixed Satellite Service
6430 M 6470 M R Fixed Satellite Service
4155 M 4195 M T Fixed Satellite Service
6480 M 6520 M R Fixed Satellite Service

S3. ORBITAL INFORMATION FOR GEOSTATIONARY SATELLITES ONLY:

S3. ORBITAL INFORMATION FOR GEOSTATIONARY SATELLITES ONLY:
a. Nominal Orbital Longitude (Degrees E/W): b. Alternate Orbital Longitude (Degrees E/W): c. Reason for orbital location selection:
11 W Replacement satellite for prior Intersputnik space
Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be station.
N/S Station-Keeping provided (Optional):
d. Toward West: Degrees E/W
0.05 Degrees Tolerance:
g. Westernmost: 85 W
e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: 60 E
i. Reason for service are selection (Optional):
Look angles below 5 degrees prohibit access to space station.

FEDERAL COMMUNICATIONS COMMISSION Page 2: NGSO Orbits
SATELLITE SPACE STATION AUTHORIZATIONS
FCC Form 312 - Schedule S: (Technical and Operational Description)

S4. ORBITAL INFORMATION FOR NON-GEOSTATIONARY SATELLITES ONLY
S4a. Total Number of Satellites in Network or System: S4c. Celestial Reference Body (Earth, Sun, Moon, etc.):
S4b. Total Number of Orbital Planes in Network or System: S4d. Orbit Epoch Date:

For each Orbital Plane Provide:
(e) Orbital (f) No. of (g) Inclination (h) Orbital (i) Apogee (km) (j) Perigee (km) (k) Right Ascension (l) Argument of Active Service Arc Range (Degrees)
Plane No. Satellites in Angle (degrees) Period of the Ascending Perigee (m) Begin (n) End Angle (o) Other
Plane (Seconds) Node (Deg.) (Degrees) Angle

S5. INITIAL SATELLITE PHASE ANGLE For each satellite in each orbital plane, provide the intital phase angle.
(a) Orbital (b) Satellite (c) Initial
Plane No. Number Phase Angle
(Degrees)

NO NGSO DATA FILED

FEDERAL COMMUNICATIONS COMMISSION Page 3: Service Areas
SATELLITE SPACE STATION AUTHORIZATIONS
FCC Form 312 - Schedule S: (Technical and Operational Description)
S6. SERVICE AREA CHARACTERISTICS for each service area provide:

(a) Service Area (b) Type of Associated (c) Service Area Diagram (d) Service Area Description. Provide list of geographic areas (state postal codes or ITU 3-ltr codes), satellites or Figure No. of
ID Station (Earth or File Name (GXT File) Service Area Diagram.
Space)

1 E Express AM44 Service Atlantic Ocean Region Satellite; Global C-band Coverage

FEDERAL COMMUNICATIONS COMMISSION Page 4: Antenna Beams
SATELLITE SPACE STATION AUTHORIZATIONS
FCC Form 312 - Schedule S: (Technical and Operational Description)
S7. SPACE STATION ANTENNA BEAM CHARACTERISTICS For each antenna beam provide:

(a) (b) Isotropic Antenna (e) (f) (g) Min. (h) Polar- (i) Polarization (j) Service Transmit Receive
Beam T/R Gain Pointing Rotational Cross- ization Alignment Rel. Area ID (k) Input (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB)
ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Losses Output Max. System Max. Saturation
(Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step
(dBi) (dBi) (dB) Power (W) EIRP Noice Gain Pt. Flux Density
(Y/N) Value Size
(dBW) Temp (k) (db/K) (dBW/m2)
6 T 22 19 0.1 30 N 1 3 100 39
6R R 20 17 0.1 30 N 1 500 -7 -92 16 1
7 T 30 27 0.1 30 N 1 3 100 47
7R R 30.5 27.5 0.1 30 N 1 500 3.5 -94 16 1
8 T 30 27 0.1 30 N 1 3 100 47
8R R 30.5 27.5 0.1 30 N 1 500 3.5 -94 16 1
9 T 30 27 0.1 30 N 1 3 100 47
9R R 30.5 27.5 0.1 30 N 1 500 3.5 -94 16 1
10 T 22 19 0.1 30 N 1 3 100 39
10R R 20 17 0.1 30 N 1 500 -7 -92 16 1
11 T 22 19 0.1 30 N 1 3 100 39
11R R 20 17 0.1 30 N 1 500 -7 -92 16 1
15 T 30 27 0.1 30 N 1 3 100 47
15R R 30.5 27.5 0.1 30 N 1 500 3.5 -94 16 1
16 T 30 27 0.1 30 N 1 3 100 47
16R R 30.5 27.5 0.1 30 N 1 500 3.5 -94 16 1
17 T 30 27 0.1 30 N 1 3 100 47
17R R 30.5 27.5 0.1 30 N 1 500 3.5 -94 16 1
18 T 30 27 0.1 30 N 1 3 100 47
18R R 30.5 27.5 0.1 30 N 1 500 3.5 -94 16 1

FEDERAL COMMUNICATIONS COMMISSION Page 5: Beam Diagrams
SATELLITE SPACE STATION AUTHORIZATIONS
FCC Form 312 - Schedule S: (Technical and Operational Description)
S8. ANTENNA BEAM DIAGRAMS For each beam pattern provide the reference to the graphic image and numerical data:
Also provide the power flux density levels in each beam that result from the emission with the highest power flux density.

(a) (b) (c) Co-or (d) GSO (e) NGSO Antenna Gain (f) GSO Antenna Max. Power Flux Density (dBW/M2/Hz)
Beam T/R Cross Ref. Contour Description Gain Contour Data At Angle of Arrival above horizontal (for emission with highest PFD)
ID Mode Polar Orbital (Figure/Table/ Exhibit) (GXT File) (g) 5 Deg (h) 10 Deg (i) 15 Deg (j) 20 Deg (k) 25 Deg
Mode ("C" Longitude
or" X") (Deg. E/W)
6 T C -11 6 GLOBAL DN.gxt -164.3 -164.2 -164 -163.9 -163.8
6R R C -11 6 GLOBAL UP.gxt
7 T C -11 AM44 7 DN.gxt -156.3 -156.2 -156 -155.9 -155.8
7R R C -11 AM44 7 UP.gxt
8 T C -11 AM44 8 DN.gxt -156.3 -156.2 -156 -155.9 -155.8
8R R C -11 AM44 8 UP.gxt
9 T C -11 AM44 9 DN.gxt -156.3 -156.2 -156 -155.9 -155.8
9R R C -11 AM44 9 UP.gxt
10 T C -11 10 GLOBAL DN.gxt -164.3 -164.2 -164 -163.9 -163.8
10R R C -11 10 GLOBAL UP.gxt
11 T C -11 11 GLOBAL DN.gxt -164.3 -164.2 -164 -163.9 -163.8
11R R C -11 11 GLOBAL UP.gxt
15 T C -11 AM44 15 DN.gxt -156.3 -156.2 -156 -155.9 -155.8
15R R C -11 AM44 15 UP.gxt
16 T C -11 AM44 16 DN.gxt -156.3 -156.2 -156 -155.9 -155.8
16R R C -11 AM44 16 UP.gxt
17 T C -11 AM44 17 DN.gxt -156.3 -156.2 -156 -155.9 -155.8
17R R C -11 AM44 17 UP.gxt
18 T C -11 AM44 18 DN.gxt -156.3 -156.2 -156 -155.9 -155.8
18R R C -11 AM44 18 UP.gxt

FEDERAL COMMUNICATIONS COMMISSION Page 6: Channels and
SATELLITE SPACE STATION AUTHORIZATIONS Transponders
FCC Form 312 - Schedule S: (Technical and Operational Description)
S9. SPACE STATION CHANNELS For each frequency channel provide: S10. SPACE STATION TRANSPONDERS For each transponder provide:
(a) (B) Assigned (c) (d) Center (e) (f) TTC (a) (b) Receive Band Transmit Band
Channel Bandwidth T/R Frequency Polarization or Comm Transponder Transponder (c) Channel (d) Beam (e) Channel (f) Beam ID
No. (kHz) Mode (MHz) (H, V, L, R) Channel (T ID Gain (dB) No. ID No.
or C)

1 40000 T 6000 L C 6 110 2 6R 1 6
2 40000 R 3675 R C 7 110 4 7R 3 7
3 40000 T 6050 L C 8 110 6 8R 5 8
4 40000 R 3725 R C 9 110 8 9R 7 9
5 40000 T 6100 L C 10 110 10 10R 9 10
6 40000 R 3775 R C 11 110 12 11R 11 11
7 40000 T 6150 L C 15 110 14 15R 13 15
8 40000 R 3825 R C 16 110 16 16R 15 16
9 40000 T 6200 L C 17 110 18 17R 17 17
10 40000 R 3875 R C 18 110 20 18R 19 18
11 40000 T 6250 L C
12 40000 R 3925 R C
13 40000 T 6350 L C
14 40000 R 4025 R C
15 40000 T 6400 L C
16 40000 R 4075 R C
17 40000 T 6450 L C
18 40000 R 4125 R C
19 40000 T 6500 L C
20 40000 R 4175 R C

FEDERAL COMMUNICATIONS COMMISSION Page 7: Digital Modulation
SATELLITE SPACE STATION AUTHORIZATIONS
FCC Form 312 - Schedule S: (Technical and Operational Description)
S11. DIGITAL MODULATION PARAMETERS For each digital emission provide:
(a) Digital (b) Emission (c) Assigned (d) No. of (e)Uncoded (f) FEC Error (g) CDMA (h) Total C/N (i) Single Entry
Mod. ID Designator Bandwidth Phases Data Rate Correction Processing Performance C/I Objective
(kHz) (kbps) Coding Rate Gain (dB) Objective (dB) (dB)

1 45K0G7D 45 4 67 0.75 6.8 30
2 128KG7D 128 4 189 0.75 6.8 30
3 40M0G7W 40000 4 66667 0.75 6.8 30
4 4M00G7W 4000 4 5925 0.75 6.8 30
5 27M0G7W 27000 4 40000 0.75 6.8 30
6 28M0G7W 28000 4 41481 0.75 6.8 30
7 34M0G7W 34000 4 50371 0.75 6.8 30
8 3M55G7W 3555 4 4444 0.75 6.8 30

FEDERAL COMMUNICATIONS COMMISSION Page 8: Analog Modulation
SATELLITE SPACE STATION AUTHORIZATIONS
FCC Form 312 - Schedule S: (Technical and Operational Description)
S12. ANALOG MODULATION PARAMETERS For each analog emission provide:
(a) (b) Emission (c) (d) Signal (e) Multi-channel Telephony (j) Video (k) Video (l) Video (m) SCPC/FM (n) Total C/N (o) Single
Analog Designator Assigned Type Channels Standard Noise- and Compander, Performance Entry C/I
(f) Ave. (g) Bottom (h) Top (i) RMS
Mod. ID Bandwidth per Carrier NTSC, Weighting SCPC/FM Preemphasis, Objective Objective
Companded Baseband Baseband Modulation
(kHz) PAL, etc. (dB) Modulation and Noise (dB) (dB)
Talker Level Freq. (MHz) Freq. (MHz) Index
Index Weighting (dB)
(dBm0)

FEDERAL COMMUNICATIONS COMMISSION Page 9: Typical Emissions
SATELLITE SPACE STATION AUTHORIZATIONS
FCC Form 312 - Schedule S: (Technical and Operational Description)
S13. TYPICAL EMISSIONS For each planned type of emission provide:
Associated Modulation ID (e) Carriers (f) Carrier (g)Noise Budget (h) Energy Receive Band (Assoc. Transmit Stn) Transmit Band (This Space Station)
Transponder ID Range per Spacing Reference (Table Dispersal
(c) Digital (d) Analog (i)Assoc. Assoc. Station Transmit EIRP (dBW) (n) Max. Power (o)Assoc.
Transponder (kHz) No.) Bandwidth
(Table S11) (Table S12) Stn. Max. Power (dBW) Flux Density Stn Rec.
(a) Start (b) End (kHz)
Antenna (dBW/m2/Hz) G/T
Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dB/K)
6 6 1 1 Ex G, LB2 51.3 -8.9 -6.9 5 7 -166 18.7
10 10 1 1 Ex G, LB2 51.3 -8.9 -6.9 5 7 -166 18.7
11 11 1 1 Ex G, LB2 51.3 -8.9 -6.9 5 7 -166 18.7
6 6 2 1 Ex G, LB4 51.3 -4.4 -2.4 9.5 11.5 -166.1 18.7
10 10 2 1 Ex G, LB4 51.3 -4.4 -2.4 9.5 11.5 -166.1 18.7
11 11 2 1 Ex G, LB4 51.3 -4.4 -2.4 9.5 11.5 -166.1 18.7
6 6 3 1 Ex G, LB13 51.3 20.3 22.3 34.5 36.5 -166 18.7
10 10 3 1 Ex G, LB13 51.3 20.3 22.3 34.5 36.5 -166 18.7
11 11 3 1 Ex G, LB13 51.3 20.3 22.3 34.5 36.5 -166 18.7
6 6 4 1 Ex G, LB5 51.3 9.4 11.4 24.2 26.2 -166.3 18.7
10 10 4 1 Ex G, LB5 51.3 9.4 11.4 24.2 26.2 -166.3 18.7
11 11 4 1 Ex G, LB5 51.3 9.4 11.4 24.2 26.2 -166.3 18.7
6 6 5 1 Ex G, LB7 51.3 17.7 19.7 32.4 34.4 -166.4 18.7
10 10 5 1 Ex G, LB7 51.3 17.7 19.7 32.4 34.4 -166.4 18.7
11 11 5 1 Ex G, LB7 51.3 17.7 19.7 32.4 34.4 -166.4 18.7
6 6 6 1 Ex G, LB9 51.3 17.9 19.9 32.6 34.6 -166.4 18.7
10 10 6 1 Ex G, LB9 51.3 17.9 19.9 32.6 34.6 -166.4 18.7
11 11 6 1 Ex G, LB9 51.3 17.9 19.9 32.6 34.6 -166.4 18.7
6 6 7 1 Ex G, LB11 51.3 18.7 20.7 33.4 35.4 -166.4 18.7
10 10 7 1 Ex G, LB11 51.3 18.7 20.7 33.4 35.4 -166.4 18.7
11 11 7 1 Ex G, LB11 51.3 18.7 20.7 33.4 35.4 -166.4 18.7
15 15 1 1 Ex G, LB1 51.4 -7.9 -5.9 12.4 14.4 -158.6 18.9
16 16 1 1 Ex G, LB1 51.4 -7.9 -5.9 12.4 14.4 -158.6 18.9
17 17 1 1 Ex G, LB1 51.4 -7.9 -5.9 12.4 14.4 -158.6 18.9
18 18 1 1 Ex G, LB1 51.4 -7.9 -5.9 12.4 14.4 -158.6 18.9
15 15 2 1 Ex G, LB3 51.4 -3.4 -1.4 17 19 -158.6 18.9
16 16 2 1 Ex G, LB3 51.4 -3.4 -1.4 17 19 -158.6 18.9
17 17 2 1 Ex G, LB3 51.4 -3.4 -1.4 17 19 -158.6 18.9
18 18 2 1 Ex G, LB3 51.4 -3.4 -1.4 17 19 -158.6 18.9

15 15 3 1 Ex G, LB14 51.4 19.8 21.8 43.5 45.5 -157 18.9
16 16 3 1 Ex G, LB14 51.4 19.8 21.8 43.5 45.5 -157 18.9
17 17 3 1 Ex G, LB14 51.4 19.8 21.8 43.5 45.5 -157 18.9
18 18 3 1 Ex G, LB14 51.4 19.8 21.8 43.5 45.5 -157 18.9
15 15 4 1 Ex G, LB8 51.3 19.6 21.6 40 42 -158.8 18.9
16 16 4 1 Ex G, LB8 51.3 19.6 21.6 40 42 -158.8 18.9
17 17 4 1 Ex G, LB8 51.3 19.6 21.6 40 42 -158.8 18.9
18 18 4 1 Ex G, LB8 51.3 19.6 21.6 40 42 -158.8 18.9
15 15 5 1 Ex G, LB10 51.3 19.8 21.8 40.2 42.2 -158.8 18.9
16 16 5 1 Ex G, LB10 51.3 19.8 21.8 40.2 42.2 -158.8 18.9
17 17 5 1 Ex G, LB10 51.3 19.8 21.8 40.2 42.2 -158.8 18.9
18 18 5 1 Ex G, LB10 51.3 19.8 21.8 40.2 42.2 -158.8 18.9
15 15 6 1 Ex G, LB12 51.3 20.6 22.6 41 43 -158.8 18.9
16 16 6 1 Ex G, LB12 51.3 20.6 22.6 41 43 -158.8 18.9
17 17 6 1 Ex G, LB12 51.3 20.6 22.6 41 43 -158.8 18.9
18 18 6 1 Ex G, LB12 51.3 20.6 22.6 41 43 -158.8 18.9
15 15 7 1 Ex G, LB6 51.4 11.3 13.3 31.7 33.7 -158.3 18.9
16 16 7 1 Ex G, LB6 51.4 11.3 13.3 31.7 33.7 -158.3 18.9
17 17 7 1 Ex G, LB6 51.4 11.3 13.3 31.7 33.7 -158.3 18.9
18 18 7 1 Ex G, LB6 51.4 11.3 13.3 31.7 33.7 -158.3 18.9
7 7 1 1 Ex G, LB1 51.4 -7.9 -5.9 12.4 14.4 -158.6 18.9
8 8 1 1 Ex G, LB1 51.4 -7.9 -5.9 12.4 14.4 -158.6 18.9
9 9 1 1 Ex G, LB1 51.4 -7.9 -5.9 12.4 14.4 -158.6 18.9
7 7 2 1 Ex G, LB3 51.4 -3.4 -1.4 17 19 -158.6 18.9
8 8 2 1 Ex G, LB3 51.4 -3.4 -1.4 17 19 -158.6 18.9
9 9 2 1 Ex G, LB3 51.4 -3.4 -1.4 17 19 -158.6 18.9
7 7 3 1 Ex G, LB14 51.4 19.8 21.8 43.5 45.5 -157 18.9
8 8 3 1 Ex G, LB14 51.4 19.8 21.8 43.5 45.5 -157 18.9
9 9 3 1 Ex G, LB14 51.4 19.8 21.8 43.5 45.5 -157 18.9
7 7 4 1 Ex G, LB8 51.3 19.6 21.6 40 42 -158.8 18.9
8 8 4 1 Ex G, LB8 51.3 19.6 21.6 40 42 -158.8 18.9
9 9 4 1 Ex G, LB8 51.3 19.6 21.6 40 42 -158.8 18.9
7 7 5 1 Ex G, LB10 51.3 19.8 21.8 40.2 42.2 -158.8 18.9
8 8 5 1 Ex G, LB10 51.3 19.8 21.8 40.2 42.2 -158.8 18.9
9 9 5 1 Ex G, LB10 51.3 19.8 21.8 40.2 42.2 -158.8 18.9
7 7 6 1 Ex G, LB12 51.3 20.6 22.6 41 43 -158.8 18.9
8 8 6 1 Ex G, LB12 51.3 20.6 22.6 41 43 -158.8 18.9
9 9 6 1 Ex G, LB12 51.3 20.6 22.6 41 43 -158.8 18.9
7 7 7 1 Ex G, LB6 51.4 11.3 13.3 31.7 33.7 -158.3 18.9

8 8 7 1 Ex G, LB6 51.4 11.3 13.3 31.7 33.7 -158.3 18.9
9 9 7 1 Ex G, LB6 51.4 11.3 13.3 31.7 33.7 -158.3 18.9

FEDERAL COMMUNICATIONS COMMISSION Page 10: TT and C
SATELLITE SPACE STATION AUTHORIZATIONS
FCC Form 312 - Schedule S: (Technical and Operational Description)
S14. Is the space station(s) controlled and monitored remotely? If Yes, provide the location and telephone number of the TT and C control point(s): Yes

Remote Control (TT C) Location(s):
S14a: Street Address:
Octyabvskaya
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
Gus-Khrustalny Russia 801501
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
+70959569526

FEDERAL COMMUNICATIONS COMMISSION Page 11:
SATELLITE SPACE STATION AUTHORIZATIONS Characteristics and
FCC Form 312 - Schedule S: (Technical and Operational Description) Certifications

S15. SPACECRAFT PHYSICAL CHARACTERISTICS:
S15a: Mass of spacecraft without fuel (kg): Spacecraft Dimensions Probability of Survival to
2327 (meters) End of Life (0.0 - 1.0)
S15b. Mass of fuel and disposables at launch (kg):
205
S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload:
2532 26.532 0.8565
S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus:
205 6.625 0.8544
S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total:
61.2 5.062 0.7318

S16. SPACECRAFT ELECTRICAL CHARACTERISTICS:
Spacecraft Electrical Power (Watts) At Electrical Power (Watts) At
Subsystem Beginning of Life End of Life
At Equinox At Solstice At Equinox At Solstice
Payload (Watts): (a): (f): (k): (p):
4410 4410 4410 4410
Bus (Watts): (b): (g): (l): (q):
1183 1095 1183 1095
Total (Watts): (c): (h): (m): (r):
5593 5505 5593 5505
Solar Array (Watts): (d): (i): (n): (s):
8354 7443 6766 6029
Depth of Battery (e) (j) (o) (t)
Discharge (%):
% % % %

S17. CERTIFICATIONS:
a. Are the power flux density limits of § 25.208 met?: X YES NO N/A
b. Are the appropriate service area coverage requirements of § 25.143(b)(ii) and (iii), or § 25.145(c)(1) and (2) met? YES NO X N/A
c. Are the frequency tolerances of § 25.202(e) and the out-of-band emission limits of § 25.202(f)(1), (2) and (3) met?
X YES NO N/A
In addition to the information required in this Form, the space station applicant is required to provide all the information specified in Section 25.114 of the
Commission's rules, 47 C.F.R § 25.114.

Document Created: 2012-07-31 09:00:38
Document Modified: 2012-07-31 09:00:38

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