Attachment Response fr Orbimage

Response fr Orbimage

REPLY submitted by Orbimage

Response from Orbimage

2005-09-01

This document pretains to SAT-MOD-20050511-00097 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2005051100097_453883

   James F. Rogers                                                     555 Eleventh Street, N.W., Suite 1000
   Direct Diak: (202) 637—2215                                         Washington, D.C. 200041804
   jim.rogers@Iw.com                                                   Tek: (202) 637—2200 Fax: (202) 687—2201
                                                                       www.lw.com


LATHAM&WATKINS«                                                        Boston
                                                                       FIRM / AFFILIATE OFFICES
                                                                                       New York
                                                                       Brussels        Northem Virginia
                                                                       Chicago         Orange County
                                                                       Frankfurt       Paris
                                                                       Hamburg         San Diego
   September 1, 2005                                                   Hong Kong       San Francisco
                                                                       London          Shanghai
                                                                       Los Angeles     Silicon Valley
   .B_Y_I{_A—N.Q                                                       Milan           Singapore
                                                                       Moscow          Tokyo
                                                                       New Jersey      Washington, D.C.

   Robert G. Nelson
   Chief, Engineering Branch
   Satellite Division
   International Bureau
   Federal Communications Commission
   Washington, DC 20554


              Re:        Application of ORBIMAGE, Inc.
                         Call Sign $2348
                         File No. SAT—MOD20050511—0097

   Dear Mr. Nelson:

              In response to your letter of August 11, 2005, concerning the above application,
   ORBIMAGE has prepared the attached letter providing the information you requested. Please
   feel free to call or email me if you have any further questions.



                                                   Very truly yours,

                                                      %&v J [<ag
                                                            3
                                                   Jamsz’é F. Rogers
                                                   ofLATHAM & WATKINS LLP

   Enclosure

   ce:        Fern Jarmulnek (International Bureau)
              Sylvia Lam (International Bureau)
              Lee F. Demitry (ORBIMAGE)
             William Lee Warren, Esq. (ORBIMAGE)
             David Kenyon (ORBIMAGE)


                                                                       !%RBIMAGE
                                                                         GLOBAL IMAGING INFORMATION




August 30, 2005




Robert G. Nelson
Chief Engineering Branch
Satellite Division
International Bureau
Federal Communications Commission
Washington, D.C. 20554

                Re:    Application of ORBIMAGE, Inc.
                       Call Sign $2348
                       File No. SAT—MOD20050511—00097

Dear Mr. Nelson:

        ORBIMAGE, Inc. (CORBIMAGE") hereby responds to your letter dated August 10, 2005
requesting supplemental information concerning the above—referenced application to modify its
existing license to add an additional satellite, OrbView—5 ("OV—5").

        The letter indicated that further clarification and additional information was needed in
order to facilitate the coordination between the Commission and NTIA. Accordingly,
ORBIMAGE was asked to supply three items ofinformation: First, the Commission requested
that ORBIMAGE provide the frequency response of the filter described in Exhibit 2, Technical
Annex, page 7 of the application and to explain whether these characteristics are the same as
those of the current constellation. Second, ORBIMAGE was asked to provide the maximum
power spectral density ("PSD") in the frequency range of 8400 MHz—8450 MHz for the
Telemetry Downlink. Finally, the letter requested that ORBIMAGE provide the crossing time of
the ascending node of OV—5.

         In response to the first inquiry, ORBIMAGE provides the filter response in the attached
Exhibit A. The OV—5 filter characteristics are not the same as those on the current constellation,
OV—3. The OV—5 x—band downlink covers a wider bandwidth (370 MHz) than the OV—3
downlink (150 MHz). In addition, the OV—3 center frequency of 8190 MHz differs from the OV—
5 center frequency of 8210 MHz. In response to the second inquiry, ORBIMAGE provides the
maximum PSD in the attached Exhibit B.

         ORBIMAGE is aware that the Commission may have a particular concern about the
potential for interference with the Deep Space Network ("DSN"). Accordingly, ORBIMAGE
examined the potential for interference with the DSN in the context of the ITU regulations.
Because the OV—5 transmitters are deactivated, except when over a ground station, the only
potential for interference is between ORBIMAGE‘s Dulles Ground station and DSN‘s Goldstone
antenna. As demonstrated in the attached exhibits, ORBIMAGE calculated the worst—case



DC\787587. 1


scenario for this potential interference and found that the interference potential is well within the
ITU‘s recommendations.

       In response to the Commission‘s third inquiry, the satellite crossing time ofthe
descending node is controlled to be 10:30 AM +/— 20 minutes. Thus, the ascending nodal
crossing time is 10:30 PM.

        If you have additional questions concerning the above—referenced application, please
contact the undersigned.




                                               Respectfully submitted,

                                                                    t




                                               William L. Warren




DCUS7587.1


                                                           EXHIBIT A

           DSN Filter Response

           Figure 1 shows the OV—5 DSN filter response. Series 1 is the ideal filter response and Series 2 is the
           actual filter response.

                                          AMPLITUDE IDEAL VS. PROTYPE


               Rord        6Q      Th        _lgsg_q     baid     baed    %;w
       h
      m




~10




                                                                                         s




                                                       FREQ MHZ

                                             Figure 1. OV—5 DSN Filter Response

           The following calculations show that the 370 Mbps wideband downlink meets the ITU Recommendation
           ITU—R SA. 1157 Protection Criteria for Deep—Space Research with at least 6.85 dB of margin.

           Power Flux Density Calculation @ 4 kHz Integration
           The NTIA and ITU PFD recommendations specify a not to exceed PFD value for all ground point
           locations. The recommendations dictate that the PFD shall be integrated over a 4 kHz bandwidth. This
           can be seen in the below equation.

           PFD=Tx(dBW) + SCAntennaGain(dB) + Losses(dB) +10* Log( V_ , D(myp2) +!90* Log(400%w> + ModLoss

           (Worst Case Scenario)
           Simulations showed that the angle between the boresight of the antenna during a contact with the Dulles,
           VA ground station and the 70—meter DSN antenna at Goldstone to be > 76. Calculations where made for
           a worst—case PFD in which the maximum gain (of angles > 76) and closest range (when both sites are in




           DC\787587.1


view) are used. The maximum amount of PFD at the ground at the downlink channel centerfrequency
becomes:

(Assuming)
Tx (dBW)                         10 Watt Transmitter = 10 dBw



                        i
Tx Frequency                     8210 MHz


                        dt
SCAntennaGain (dB)               3 dBi Antenna Gain

                        nb
Losses (dB)                      —8 dB Filter + Cable + Gimbal
D{m)                    ar
                        db       2027 km slant range ~ 2,027,000 m (closest approach)
BW (MHz)                         370 MHz
                        iob


Modulation Loss                  0 dB

PFD = (10 dBW) + (3dB) + (—8 dB) + (—137.13 dB/m*) + (—49.66 dB/4kHz) + (0 dB)

PFD = ~181.79 dB(W/m"/4kHz)
Converting the 4 kHz BW to 1 Hz BW:;

10 log (4000) = 36.02 dB

PFD = (—181.79 dBW/m"/4kHz) — (36.02 dB)

PFD = —217.81 dB(W/m*/Hz)
The ITU Recommendation ITU—R S$A.1157 Protection Criteria for Deep—Space Research states that the
maximum allowable interference power spectral flux—density into a DSN receiver is —255.1 dB(W/im*/Hz).

The rejection required in the Deep—Space Research band is:

Regquired Rejection = Max SC PFD — DSN specification

Required Rejection = (—217.81 dB(W/m*/Hz)) — (— 255.1 dB(W/m"/Hz))
Required Rejection = 37.29 dB

The spectral density of the signal = P/SR Sin@(mAf/SRY/(mTAf/SR)"; where SR is the symbol rate and Af is
the delta frequency from center the frequency.

Freq               (Ffo/SR)             10 tog [(sin®\/x"] (dB)
8400                1.027027             —31.60
8410                1.081081             —22.59
8420                11351                18.75
8430                1189189              16.48
8440                1.243243             15.03
8450                1.297297             4410
The required filter attenuation by frequency is:

Regquired filter attenuation = 37.29 dB + 10 log((sin®x}/x") in the 8400 to 8450 MHz band
Regquired filter attenuation @ 8400 MHz = (37.29 dB) + (—31.60 dB)
Required filter attenuation @ 8400 MHz = 5.69 dB
Actual filter attenuation @ 8400 MHz = 21 dB

Margin @ 8400 MHz = 15.31 dB




DC\787587.1


Required filter attenuation @ 8410 MHz = (37.29 dB) + (—22.59 dB)
Required filter attenuation @ 8410 MHz = 14.70 dB
Actual filter attenuation @ 8410 MHz = 24 dB

Margin @ 8410 MHz = 9.30 dB


Required filter attenuation @ 8420 MHz = (37.29 dB) + (—18.75 dB)
Required filter attenuation @ 8420 MHz = 19.15 dB
Actual filter attenuation @ 8420 MHz = 26 dB

Margin @ 8420 MHz = 6.85 dB

Required filter attenuation @ 8430 MHz = (37.29 dB) + (—16.48 dB)
Required filter attenuation @ 8430 MHz = 20.81 dB
Actual filter attenuation @ 8430 MHz = 28 dB

Margin @ 8430 MHz =7.19 dB

Required filter attenuation @ 8440 MHz = (37.29 dB) + (—15.03 dB)
Required filter attenuation @ 8440 MHz = 22.26 dB
Actual filter attenuation @ 8440 MHz = 31 dB

Margin @ 8440 MHz = 8.74 dB

Required filter attenuation @ 8450 MHz = (37.29 dB) + (—14.10 dB)
Required filter attenuation @ 8450 MHz = 23.19 dB
Actual filter attenuation @ 8450 MHz = 33 dB

Margin @ 8450 MHz = 9.81 dB




DC\787387.1


                                             EXHIBIT B

Power Spectral Density in the frequency range of 8400 to 8450 MHz for the telemetry downlink

The PSD of the telemetry downlink is at the most —70 dBc in the 8400 to 8450 MHz range. This is due to
spurious emissions rather than modulated data. The following calculations show that the telemetry
downlink meets the ITU Recommendation ITU—R SA. 1157 Protection Criteria for Deep—Space Research
with 8.09 dB of margin.

Power Flux Density Calculation @ 4 kHz Integration
The ITU PFD recommendations specify a not to exceed PFD value for all ground point locations. The
recommendations dictate that the PFD shall be integrated over a 4 kHz bandwidth. This can be seen in
the below equation:

PFD=Tx(dBW) + SCAntennaGain{dB) + Losses(dB)+10* Log( ;, , Dimp2) +19* Lng(400%w) + ModLoss

Simulations showed that the closest slant range to the 70 Meter antenna at Goldstone (when both
Goldstone and the Dulles ground site are in view) is 2027 km. This is the only time that the TLM
Transmitter can be on. The maximum amount of PFD at the ground at the downlink channel center
frequency becomes:

(Assuming)
Tx                              2 Watt Transmitter = 3 dBW
                          ut




Tx Frequency                    8394 MHz
                          di




SC Antenna Gain                 0 dBi Maximum Antenna Gain at 8400 MHz
                          db




Losses                          ~11 dB (Attenuator + Cable + Coupler)
                          db




D                               2027 km slant range ~ 2,027,000 m (closest approach)
                          ar




BW                              64 kHz
                          W




Modulation Loss                 0 dB

PFD = (3 dBW) + (0dB) + (—11 dB) + (—137.13 dB/m") + (—12.04 dB/4kHz) + (0 dB)
PFD = —157.17 dB(W/m*/4kHz)
The TLM signal is —70 dBc at 8400 to 8450 MHz. This is the spurious behavior of the transmitter; the data
PSD at this distance from the center frequency is lower.

PSD at 8400 MHz = PFD + TLM PSD at 8400 MHz

PFD at 8400 MHz = (—157.17 dBW/m*/4kHz) + (—70 dB)

PFD at 8400 MHz = —227.17 dB(W/m"/4kHz)

The ITU Recommendation ITU—R SA. 1157 Protection Criteria for Deep—Space Research states that the
maximum allowable interference power spectral flux—density into a DSN receiver is —255.1 dB(W/mlez),

Converting the 4 kHz BW to 1 Hz BW:

10 log (4000) = 36.02 dB

PFD at 8400 MHz = (—227.17 dBW/m*/4kHz) — (36.02 dB)

PFD at 8400 MHz = —263.19 dB(W/m*/Hz)

Margin to ITU—R SA. 1157 = (—263.19 dB(W/im"/H2)) — (—255.1 dB(W/m"/H2z))

DC\787587.1


.   Margin to ITU—R SA.1157 = 8.09 dB




     DC\787587.1



Document Created: 2005-09-08 09:14:25
Document Modified: 2005-09-08 09:14:25

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