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Resolution 609 (WRC-03) Consultation Meeting 2-4 June 2004 Record of Decisions Taken at the Second Resolution 609 (WRC-03) Consultation Meeting (Ottawa, 2-4 June 2004) The second Resolution 609 (WRC-03) Consultation Meeting was convened, pursuant to the requirements of Resolution 609 (WRC-03), at the facilities of the Telesat Canada in Ottawa, Canada, from 2-4 June 2004. A list of participants is available on the Resolution 609 Forum page on the ITU web site. Approximately 55 delegates from government and industry, along with a representative of the Radiocommunication Bureau, attended the meeting. The following actions were taken: 1. The Meeting agreed to a modification to the Terms of Reference that were adopted in December 2003 to address the subjects of the preparation of the Report to the Radiocommunication Bureau, treatment at future Consultation Meetings of system characteristics and commitments pursuant to the Annex to Resolution 609 (WRC-03) that had been supplied pursuant to §§ 11 b) and c) to a previous Consultation Meeting, and the matters relating to the distribution of submissions for Consultation Meetings. A copy of the modified Terms of Reference has been posted to the Resolution 609 Forum that is maintained by the BR on the ITU web site (http://www.itu.int/ITU-R/space/res609/). 2. The Meeting decided that the third Resolution 609 (WRC-03) Consultation Meeting will be convened in Brussels, Belgium, for a period of three working days, tentatively in June 2005. 3. The Meeting agreed to a modification to the format for the provision of RNSS system characteristics to the Consultation Meeting. The revised format is contained in Attachment 1 hereto. The meeting agreed that under the revised format, as under the format adopted initially in December 2003, each administration should also provide a new Section I-9 (see Attachment 1) containing the result of the epfd calculation for each RNSS individual system, available in MS Excel format (see Attachment 2 at Template, Sheet 1) using 5 degree steps in latitude and longitude. For non-GSO systems, administrations should also provide the time step resolution and the number of time steps simulated. a. It was agreed that if the calculation of the aggregate epfd of all RNSS systems is within 2 dB of the epfd limit (121.5 dBW/m 2 /MHz), the results for each RNSS system should be provided in 1 degree steps (see Attachment 2 at Template, Sheet 2). b. The system spectral adjustment factors (SAF) provided under Section I-8 should be in MS Excel format (see Attachment 2 at Template, Sheet 3).

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  • Resolution 609 (WRC-03) Consultation Meeting 2-4 June 2004

    Record of Decisions Taken at the Second Resolution 609 (WRC-03) Consultation Meeting

    (Ottawa, 2-4 June 2004)

    The second Resolution 609 (WRC-03) Consultation Meeting was convened, pursuant to the requirements of Resolution 609 (WRC-03), at the facilities of the Telesat Canada in Ottawa, Canada, from 2-4 June 2004. A list of participants is available on the Resolution 609 Forum page on the ITU web site. Approximately 55 delegates from government and industry, along with a representative of the Radiocommunication Bureau, attended the meeting. The following actions were taken: 1. The Meeting agreed to a modification to the Terms of Reference that were adopted in December 2003 to address the subjects of the preparation of the Report to the Radiocommunication Bureau, treatment at future Consultation Meetings of system characteristics and commitments pursuant to the Annex to Resolution 609 (WRC-03) that had been supplied pursuant to 11 b) and c) to a previous Consultation Meeting, and the matters relating to the distribution of submissions for Consultation Meetings. A copy of the modified Terms of Reference has been posted to the Resolution 609 Forum that is maintained by the BR on the ITU web site (http://www.itu.int/ITU-R/space/res609/). 2. The Meeting decided that the third Resolution 609 (WRC-03) Consultation Meeting will be convened in Brussels, Belgium, for a period of three working days, tentatively in June 2005. 3. The Meeting agreed to a modification to the format for the provision of RNSS system characteristics to the Consultation Meeting. The revised format is contained in Attachment 1 hereto. The meeting agreed that under the revised format, as under the format adopted initially in December 2003, each administration should also provide a new Section I-9 (see Attachment 1) containing the result of the epfd calculation for each RNSS individual system, available in MS Excel format (see Attachment 2 at Template, Sheet 1) using 5 degree steps in latitude and longitude. For non-GSO systems, administrations should also provide the time step resolution and the number of time steps simulated.

    a. It was agreed that if the calculation of the aggregate epfd of all RNSS systems is within 2 dB of the epfd limit (121.5 dBW/m2/MHz), the results for each RNSS system should be provided in 1 degree steps (see Attachment 2 at Template, Sheet 2).

    b. The system spectral adjustment factors (SAF) provided under Section I-8 should be in MS Excel format (see Attachment 2 at Template, Sheet 3).

  • 4. The Meeting agreed with respect to the systems that provided technical characteristics to the June 2004 Consultation Meeting that it would not be necessary for such same information to be provided anew to the Third Consultation Meeting. Instead, where revisions were necessitated by the revision to the characteristics format referred to in No. 3 above, the Meeting agreed that such revisions are adequately reflected in the system characteristics statements for the submitting systems that are included in Attachment 3 hereto.

    5. The Meeting compared the results from five different tools for determining the aggregate epfd produced by all considered RNSS systems. These tools were found to be in agreement to within 0.15 dB at all frequencies. The Meeting was satisfied with this degree of closeness of the results of calculations performed using the five calculation tools. 6. The Meeting performed two calculations of the maximum aggregate epfd produced by all RNSS systems that provided characteristics to the June 2004 Meeting. One calculation was performed for all systems for which information was provided on or before the 2 February 2004 deadline for system characteristics submissions, and a second calculation was performed for all systems for which information was provided on or before the 2 February 2004 deadline, and for several systems for which information was submitted after the 2 February 2004 deadline. 7. The Meeting determined that under both of its aggregate epfd calculations, the maximum epfd of all satellites associated with the referenced RNSS systems was 125.7 dB (W/m2/MHz), i.e. 4.2 dB below the Resolution 609 limit of 121.5 dBW/m2/MHz. The meeting noted that in both cases, this result is based on the use of worst-case assumptions in terms of interference from RNSS into ARNS. For example, in the case of non-GSO RNSS systems using circular orbits, the epfd at a given latitude is considered equal for any longitude to that of the worst-case longitude. 8. The Meeting agreed on a Report to the Radiocommunication Bureau that contains the results of the calculation mentioned in Nos. 6 and 7 above, and directed that this Report be communicated to the BR in the manner contemplated in 14 of the modified Terms of Reference. A copy of the Report to the Radiocommunication Bureau has been posted to the Resolution 609 Forum that is maintained by the BR on the ITU web site (http://www.itu.int/ITU-R/space/res609/). 9. The Meeting agreed that it is important, for the orderly operation of the Resolution 609 (WRC-03) consultation process and to ensure the achievement of accurate calculation results, that administrations providing information to Consultation Meetings comply with the deadlines established in the Terms of Reference. 10. The Meeting received for information a copy of the BR determination of compliance with the pfd criterion as per instructs BR 2 from Resolution 609 (WRC-03). After some discussion, the Meeting noted the document. 11. Discussion took place regarding the requirement to comply with the provisional aggregate pfd limit (-115 dB(W/m2/MHz)) in No. 5.328A (WRC-2000) of the Radio Regulations, which was put into place by WRC-2000. Although not within the terms of reference of the Resolution 609 Consultation Meeting, the issue is closely related to the subject of epfd determination, as

    2

  • WRC-03 replaced the provisional aggregate pfd limit with the epfd criterion. GSO RNSS networks which requested coordination before the last day of WRC-03 were required to provide a value of the aggregate pfd with the coordination information. The question was raised as to whether there remained a need for RNSS networks to demonstrate compliance with the provisional aggregate pfd limit. For coordination requests and notifications made after 1 January 2004, the Bureau explained that with the changes to Appendix 4 made by WRC-03, there is now a requirement to provide a commitment of compliance with the per-satellite pfd level (item A.17.a) and no requirement for any further commitment regarding the provisional aggregate pfd limit. Furthermore, the Bureau explained that administrations which gave a commitment prior to the end of WRC-03 that they would comply with the provisional aggregate pfd limit would not be required to take any further action with regard to that limit. The interested participants were appreciative of the opportunity to meet with the Bureau and receive this useful clarification with regard to this matter. 12. The Meeting expressed its gratitude to Telesat Canada for hosting the Meeting and providing extraordinary hospitality to the participants. List of Attachments Attachment 1 (Word document) input format for RNSS system characteristics. Attachment 2 (Excel spreadsheet):

    Sheet 1. Template for new section I-9 of Attachment 1, latitude/longitude format for individual system epfd calculation results (5 steps).

    Sheet 2. Template for new section I-9 of Attachment 1, longitude/latitude (note orientation

    change) format for individual system epfd calculation results (1 steps). Sheet 3. Template for section I-8 of Attachment 1, spectral adjustment factors (SAF)

    relative to the worst 1MHz. Attachment 3 (Word document) RNSS system characteristics using revised input format Attachment 4 (Excel spreadsheet): Simulated per-system epfd

    3

  • ATTACHMENT 1

    List of RNSS system characteristics to be provided to the Consultation Meeting per Item 11 c) of the Terms of Reference

    I RNSS systems characteristics I-1 RNSS ITU publication reference RNSS network name BR Network ID ITU Publication reference IFIC

    AR11/A/... API/A/... AR11/C/... CR/C/...

    I-2 Non-GSO satellite system constellation parameters N: number of space stations of the non-GSO system K: number of orbital planes h: satellite altitude above the Earth (at apogee1) (km) hP: satellite altitude above the Earth at perigee1 (km) I: inclination angle of the orbital plane above the Equator (degrees).

    Satellite index I

    RAAN i,0 (degrees)

    Argument of latitude ui,0 (degrees)

    Argument of perigee of the

    non-GSO system1 :

    1 ... ... 2 ... ... ... ... ... N ... ...

    1Note: Applicable to non-GSO systems with elliptical orbit. I-3 GSO satellite system longitude LonGSOi : longitude of each of the GSO satellites (degrees).

    4

  • I-4 Maximum circular orbit non-GSO space station pfd versus the elevation angle at 40,000 feet above the Earths surface (worst 1 MHz)

    Elevation angle (each 1)

    Pfd (dB(W/(m2/MHz)))

    4 pfd (4) 3 pfd (3) 90 pfd (90)

    I-5 Maximum GSO space station pfd versus latitude and longitude at 40,000 feet above the Earths surface (worst 1 MHz) Longitude (each 1) 0 1 360 Latitude (each 1) Maximum pfd dB(W/m2) in worst 1 MHz

    90 pfd (0, 90) 89 90 pfd (360, 90)

    I-6 Maximum elliptical orbit non-GSO space station off-axis EIRP density and additional satellite antenna pointing information (worst 1MHz) For elliptical orbit non-GSO systems, the following information is needed in order to calculate the epfd matrix: a) Satellite antenna pointing direction and other operational information to be used in

    calculating epfd values. b) Off-axis EIRP density:

    Off-axis Angle (each 1)

    EIRP density (dBW in worst 1MHz)

    0 Eirp (0) 1 Eirp (1)

    5

  • I-7 Frequency/Satellite Matrix For non-GSO constellations where each satellite transmits different signals and/or at different central frequencies,

    Satellite index I

    Transmitted Signal Central

    Frequency (MHz)

    Attenuation of transmitted signal in

    worst 1 MHz (dB)1 N

    I-8 GSO/non-GSO satellite system spectrum The level of spectrum emission in each 1 MHz relative to the spectrum value at the worst 1 MHz of the whole band (1 164-1 215 MHz) is provided below as the Spectral Adjustment Factor (SAF) in dB.

    Normalised Signal Power Spectrum

    Center Frequency

    (MHz)

    SAF (dB)

    Center Frequency

    (MHz)

    SAF (dB)

    Center Frequency

    (MHz)

    SAF (dB)

    Center Frequency

    (MHz)

    SAF (dB)

    1164 1177 1190 1203 1165 1178 1191 1204 1166 1179 1192 1205 1167 1180 1193 1206 1168 1181 1194 1207 1169 1182 1195 1208 1170 1183 1196 1209 1171 1184 1197 1210 1172 1185 1198 1211 1173 1186 1199 1212 1174 1187 1200 1213 1175 1188 1201 1214 1176 1189 1202 1215

    6

  • I-9 Results of the epfd calculation for an individual system in the worst 1 MHz of the 1 164-1 215 MHz band Longitude (each 5)2 0 5 360 Latitude (each 5)2 Maximum epfd dB(W/m2) in worst 1 MHz

    90 Epfd (0, 90) 85 90 epfd (360, 90)

    Additional simulation data for non-GSO systems only: Time step (sec) Number of time steps

    II. Technical Contact Person Name: Tel./Fax: E-mail Address:

    ________________________________ 2 See Record of 2-4 June 2004 Consultation Meeting.

    7

  • ATTACHMENT 2

    Microsoft Excel Worksheet

    8

  • ATTACHMENT 3

    "Attachment3 on RNSS systems input c

    9

  • ATTACHMENT 4

    "Att4 - Per-system epfd matrix (5).xls"

    10

    Sheet 1.

    Sheet 2.

    Sheet 3.

    ATTACHMENT 3

    List of Table 2 RNSS system characteristics

    IMSATNAV-2

    I-1RNSS ITU publication reference

    RNSS network name

    BR Network ID

    ITU Publication reference

    IFIC

    MSATNAV-21

    100500321

    API/A/1182

    2415 (API) + 2490 (Notification Part II-S)

    I-2MSATNAV-2 satellite system constellation parameters

    N=27: number of space stations of the non-GSO system (9 per plane)

    K=3:number of orbital planes

    H=23616 km:satellite altitude above the Earth (km)

    I=56:inclination angle of the orbital plane above the Equator (degrees).

    Satellite indexI

    RAAN(i,0 (degrees)

    Argument of latitude ui,0 (degrees)

    Satellite indexI

    RAAN(i,0 (degrees)

    Argument of latitude ui,0 (degrees)

    1

    0

    0

    15

    120

    213.3

    2

    0

    40

    16

    120

    253.3

    3

    0

    80

    17

    120

    293.3

    4

    0

    120

    18

    120

    333.3

    5

    0

    160

    19

    240

    26.6

    6

    0

    200

    20

    240

    66.6

    7

    0

    240

    21

    240

    106.6

    8

    0

    280

    22

    240

    146.6

    9

    0

    320

    23

    240

    186.6

    10

    120

    13.3

    24

    240

    226.6

    11

    120

    53.3

    25

    240

    266.6

    12

    120

    93.3

    26

    240

    306.6

    13

    120

    133.3

    27

    240

    346.6

    14

    120

    173.3

    I-4Maximum MSATNAV-2 space station pfd versus the elevation angle at 40000 feet above the Earths surface (worst 1 MHz)

    Elevation angle

    (each 1)

    Pfd(dB(W/(m2/MHz)))

    Elevation angle

    (each 1)

    Pfd(dB(W/(m2/MHz)))

    Elevation angle

    (each 1)

    Pfd(dB(W/(m2/MHz)))

    -4

    -135.90

    28

    -134.22

    60

    -133.70

    -3

    -135.89

    29

    -134.16

    61

    -133.76

    -2

    -135.86

    30

    -134.10

    62

    -133.82

    -1

    -135.83

    31

    -134.06

    63

    -133.88

    0

    -135.80

    32

    -134.02

    64

    -133.94

    1

    -135.76

    33

    -133.98

    65

    -134.00

    2

    -135.72

    34

    -133.94

    66

    -134.08

    3

    -135.68

    35

    -133.90

    67

    -134.16

    4

    -135.64

    36

    -133.86

    68

    -134.24

    5

    -135.60

    37

    -133.82

    69

    -134.32

    6

    -135.56

    38

    -133.78

    70

    -134.40

    7

    -135.52

    39

    -133.74

    71

    -134.48

    8

    -135.48

    40

    -133.70

    72

    -134.56

    9

    -135.44

    41

    -133.66

    73

    -134.64

    10

    -135.40

    42

    -133.62

    74

    -134.72

    11

    -135.34

    43

    -133.58

    75

    -134.80

    12

    -135.28

    44

    -133.54

    76

    -134.86

    13

    -135.22

    45

    -133.50

    77

    -134.92

    14

    -135.16

    46

    -133.48

    78

    -134.98

    15

    -135.10

    47

    -133.46

    79

    -135.04

    16

    -135.02

    48

    -133.44

    80

    -135.10

    17

    -134.94

    49

    -133.42

    81

    -135.14

    18

    -134.86

    50

    -133.40

    82

    -135.18

    19

    -134.78

    51

    -133.42

    83

    -135.22

    20

    -134.70

    52

    -133.44

    84

    -135.26

    21

    -134.64

    53

    -133.46

    85

    -135.30

    22

    -134.58

    54

    -133.48

    86

    -135.30

    23

    -134.52

    55

    -133.50

    87

    -135.30

    24

    -134.46

    56

    -133.54

    88

    -135.30

    25

    -134.40

    57

    -133.58

    89

    -135.30

    26

    -134.34

    58

    -133.62

    90

    -135.30

    27

    -134.28

    59

    -133.66

    I-8MSATNAV-2 satellite system spectrum

    The level of spectrum emission in each 1 MHz relative to the spectrum value at the worst 1MHz of the whole band (1164-1215MHz) is provided below as the Spectral Adjustment Factor (SAF) in dB.

    Normalised Signal Power Spectrum

    Center Frequency(MHz)

    SAF(dB)

    Center Frequency(MHz)

    SAF(dB)

    Center Frequency(MHz)

    SAF(dB)

    Center Frequency(MHz)

    SAF(dB)

    1164

    -15.32

    1177

    -0.04

    1190

    -11.68

    1203

    -2.37

    1165

    -19.23

    1178

    -0.32

    1191

    -10.70

    1204

    -1.33

    1166

    -29.15

    1179

    -0.87

    1192

    -10.49

    1205

    -0.61

    1167

    -20.83

    1180

    -1.71

    1193

    -11.00

    1206

    -0.17

    1168

    -13.60

    1181

    -2.90

    1194

    -12.36

    1207

    -0.01

    1169

    -9.41

    1182

    -4.48

    1195

    -14.99

    1208

    -0.10

    1170

    -6.52

    1183

    -6.60

    1196

    -20.35

    1209

    -0.46

    1171

    -4.40

    1184

    -9.49

    1197

    -29.46

    1210

    -1.11

    1172

    -2.81

    1185

    -13.75

    1198

    -17.55

    1211

    -2.08

    1173

    -1.64

    1186

    -21.38

    1199

    -11.77

    1212

    -3.41

    1174

    -0.81

    1187

    -26.91

    1200

    -8.18

    1213

    -5.20

    1175

    -0.28

    1188

    -17.61

    1201

    -5.65

    1214

    -7.59

    1176

    -0.03

    1189

    -13.70

    1202

    -3.78

    1215

    -10.92

    I-9 Results of the epfd calculation for MSATNAV-2 in the worst 1 MHz of the 1164-1215MHz band

    See attachment 4

    Additional simulation data for non-GSO systems only:

    Time step (sec)

    30 s

    Number of time steps

    2880

    Technical Contact Person

    Name: de BAILLIENCOURT Hugues

    Tel./Fax: +33 2 98 34 12 32/+33 2 98 34 12 30

    E-mail Address: [email protected]

    IINAVSTAR GPS

    II-1RNSS ITU publication reference

    RNSS network name

    BR Network ID

    ITU Publication reference

    IFIC

    NAVSTAR GPS

    100543934

    API/A/1353

    2422

    II-2GPS satellite system constellation parameters

    N = 28: number of space stations of the non-GSO system

    K = 6:number of orbital planes

    h = 20181.56:satellite altitude above the Earth (km)

    I = 55:inclination angle of the orbital plane above the Equator (degrees).

    Satellite indexI

    RAAN(i,0 (degrees)

    Argument of latitude ui,0 (degrees)

    1

    0

    0

    2

    0

    90

    3

    0

    180

    4

    0

    270

    5

    60

    60

    6

    60

    150

    7

    60

    240

    8

    60

    330

    9

    120

    120

    10

    120

    210

    11

    120

    300

    12

    120

    30

    13

    180

    180

    14

    180

    270

    15

    180

    0

    16

    180

    90

    17

    240

    240

    18

    240

    330

    19

    240

    60

    20

    240

    150

    21

    300

    300

    22

    300

    30

    23

    300

    120

    24

    300

    210

    25

    360

    10

    26

    360

    100

    27

    360

    190

    28

    360

    280

    II-4Maximum GPS space station pfd versus the elevation angle at 40000 feet above the Earths surface (worst 1 MHz)

    (The pfd values for negative elevation angles assume that the Earth has no effect on radio propagation.)

    Elevation angle (each 1)

    Pfd(dB(W/(m2/MHz)))

    4

    -142.4

    3

    -142.4

    -2

    -142.3

    -1

    -142.3

    0

    -142.3

    1

    -142.2

    2

    -142.2

    3

    -142.1

    4

    -142.1

    5

    -142.1

    6

    -142.0

    7

    -142.0

    8

    -141.9

    9

    -141.9

    10

    -141.9

    11

    -141.8

    12

    -141.8

    13

    -141.7

    14

    -141.7

    15

    -141.7

    16

    -141.6

    17

    -141.6

    18

    -141.5

    19

    -141.5

    20

    -141.4

    21

    -141.4

    22

    -141.3

    23

    -141.3

    24

    -141.3

    25

    -141.2

    26

    -141.2

    27

    -141.1

    28

    -141.1

    29

    -141.0

    30

    -141.0

    31

    -140.9

    32

    -140.9

    33

    -140.8

    34

    -140.8

    35

    -140.7

    36

    -140.7

    37

    -140.6

    38

    -140.6

    39

    -140.5

    40

    -140.5

    41

    -140.4

    42

    -140.4

    43

    -140.4

    44

    -140.3

    45

    -140.3

    46

    -140.3

    47

    -140.2

    48

    -140.2

    49

    -140.2

    50

    -140.2

    51

    -140.2

    52

    -140.2

    53

    -140.2

    54

    -140.2

    55

    -140.2

    56

    -140.3

    57

    -140.3

    58

    -140.3

    59

    -140.4

    60

    -140.4

    61

    -140.5

    62

    -140.5

    63

    -140.5

    64

    -140.6

    65

    -140.6

    66

    -140.6

    67

    -140.6

    68

    -140.6

    69

    -140.5

    70

    -140.5

    71

    -140.5

    72

    -140.5

    73

    -140.5

    74

    -140.5

    75

    -140.4

    76

    -140.4

    77

    -140.4

    78

    -140.4

    79

    -140.4

    80

    -140.4

    81

    -140.5

    82

    -140.5

    83

    -140.5

    84

    -140.5

    85

    -140.5

    86

    -140.5

    87

    -140.5

    88

    -140.6

    89

    -140.6

    90

    -140.6

    II-8GPS satellite system spectrum

    The level of spectrum emission in each 1 MHz relative to the spectrum value at the worst 1MHz of the whole band (1164-1215MHz) is provided below as the Spectral Adjustment Factor (SAF) in dB.

    Normalised Signal Power Spectrum

    Center Frequency(MHz)

    SAF(dB)

    Center Frequency(MHz)

    SAF(dB)

    Center Frequency(MHz)

    SAF(dB)

    Center Frequency(MHz)

    SAF(dB)

    1164

    -15.7

    1177

    0.0

    1190

    -13.8

    1203

    -18.6

    1165

    -19.7

    1178

    -0.3

    1191

    -13.3

    1204

    -20.3

    1166

    -33.5

    1179

    -0.9

    1192

    -13.6

    1205

    -23.1

    1167

    -21.7

    1180

    -1.8

    1193

    -14.7

    1206

    -28.5

    1168

    -14.0

    1181

    -3.0

    1194

    -16.8

    1207

    -46.8

    1169

    -9.6

    1182

    -4.7

    1195

    -20.3

    1208

    -31.4

    1170

    -6.7

    1183

    -6.9

    1196

    -26.8

    1209

    -25.3

    1171

    -4.5

    1184

    -10.0

    1197

    -47.2

    1210

    -22.5

    1172

    -2.9

    1185

    -14.5

    1198

    -26.1

    1211

    -21.2

    1173

    -1.7

    1186

    -23.0

    1199

    -21.3

    1212

    -20.8

    1174

    -0.8

    1187

    -30.4

    1200

    -19.0

    1213

    -21.2

    1175

    -0.3

    1188

    -19.1

    1201

    -18.0

    1214

    -22.5

    1176

    0.0

    1189

    -15.4

    1202

    -17.9

    1215

    -25.0

    II-9 Results of the epfd calculation for GPS in the worst 1 MHz of the 1164-1215MHz band

    See Attachment 4

    Additional simulation data for non-GSO systems only:

    Time step (sec)

    60

    Number of time steps

    1441

    Technical Contact Person

    Name: Mr. James R. Jameson

    Tel./Fax: +1-310-336-2845/+1-310-336-7500

    E-mail Address: [email protected]

    IIIGLONASS-M

    III-1RNSS ITU publication reference

    RNSS network name

    ID

    ITU Publication reference

    IFIC

    GLONASS-M

    92540003

    API/A/2264

    2469

    III-2GLONASS-M satellite system constellation parameters

    N: 24-number of space stations of the non-GSO system

    K:3-number of orbital planes

    h:19100-satellite altitude above the Earth (km)

    I:64.8-inclination angle of the orbital plane above the Equator (degrees)

    Satellite indexI

    RAAN(i,0 (degrees)

    Argument of latitude ui,0 (degrees)

    1

    335

    145

    2

    335

    100

    3

    335

    55

    4

    335

    10

    5

    335

    -35

    6

    335

    -80

    7

    335

    -125

    8

    335

    -170

    9

    95

    160

    10

    95

    115

    11

    95

    70

    12

    95

    25

    13

    95

    -20

    14

    95

    -65

    15

    95

    -110

    16

    95

    -155

    17

    215

    175

    18

    215

    130

    19

    215

    85

    20

    215

    40

    21

    215

    -5

    22

    215

    -50

    23

    215

    -95

    24

    215

    -140

    III-4Maximum GLONASS-M space station pfd versus the elevation angle at 40000 feet above the Earths surface (worst 1 MHz)

    Elevation angle (each 1)

    pfd(dB(W/(m2/MHz)))

    Elevation angle (each 1)

    pfd(dB(W/(m2/MHz)))

    -4

    -133.342

    44

    -132.195

    -3

    -133.303

    45

    -132.209

    -2

    -133.264

    46

    -132.239

    -1

    -133.225

    47

    -132.273

    0

    -133.185

    48

    -132.307

    1

    -133.146

    49

    -132.341

    2

    -133.107

    50

    -132.378

    3

    -133.068

    51

    -132.409

    4

    -133.029

    52

    -132.445

    5

    -132.990

    53

    -132.482

    6

    -132.951

    54

    -132.522

    7

    -132.912

    55

    -132.560

    8

    -132.873

    56

    -132.598

    9

    -132.835

    57

    -132.637

    10

    -132.796

    58

    -132.676

    11

    -132.757

    59

    -132.719

    12

    -132.719

    60

    -132.765

    13

    -132.681

    61

    -132.816

    14

    -132.643

    62

    -132.874

    15

    -132.605

    63

    -132.930

    16

    -132.567

    64

    -132.986

    17

    -132.530

    65

    -133.047

    18

    -132.493

    66

    -133.096

    19

    -132.456

    67

    -133.144

    20

    -132.419

    68

    -133.192

    21

    -132.390

    69

    -133.243

    22

    -132.363

    70

    -133.295

    23

    -132.336

    71

    -133.342

    24

    -132.309

    72

    -133.390

    25

    -132.284

    73

    -133.439

    26

    -132.259

    74

    -133.488

    27

    -132.234

    75

    -133.538

    28

    -132.211

    76

    -133.588

    29

    -132.187

    77

    -133.638

    30

    -132.167

    78

    -133.693

    31

    -132.154

    79

    -133.746

    32

    -132.142

    80

    -133.800

    33

    -132.132

    81

    -133.814

    34

    -132.122

    82

    -133.828

    35

    -132.119

    83

    -133.842

    36

    -132.123

    84

    -133.858

    37

    -132.127

    85

    -133.874

    38

    -132.133

    86

    -133.891

    39

    -132.140

    87

    -133.909

    40

    -132.150

    88

    -133.927

    41

    -132.160

    89

    -133.946

    42

    -132.171

    90

    -133.966

    43

    -132.183

    III-7GLONASS-M Frequency/Satellite Matrix

    Each GLONASS-M satellite transmits its signals at different central frequencies as described in the following table :

    Satellite indexI

    Transmitted Signal

    Central

    Frequency (MHz)

    Attenuation of transmitted signal in worst 1 MHz (dB)

    1

    1203.1875

    6

    2

    1202.76563

    3.8

    3

    1202.34375

    1.7

    4

    1201.92188

    0.4

    5

    1203.1875

    6

    6

    1202.76563

    3.8

    7

    1202.34375

    1.7

    8

    1201.92188

    0.4

    9

    1201.5

    0

    10

    1201.07813

    0.4

    11

    1200.65625

    1.7

    12

    1200.23438

    3.8

    13

    1201.5

    0

    14

    1201.07813

    0.4

    15

    1200.65625

    1.7

    16

    1200.23438

    3.8

    17

    1199.8125

    6

    18

    1199.39063

    7.3

    19

    1198.96875

    7.5

    20

    1198.54688

    7.7

    21

    1199.8125

    6

    22

    1199.39063

    7.3

    23

    1198.96875

    7.5

    24

    1198.54688

    7.7

    III-8GLONASS-M satellite system spectrum

    The level of spectrum emission in each 1 MHz relative to the spectrum value at the worst 1 MHz of the whole band (1164-1215 MHz) is provided below as the Spectral Adjustment Factor (SAF) in dB.

    Normalized Signal Power Spectrum

    Center Frequency (MHz)

    SAF

    (dB)

    Center Frequency (MHz))

    SAF

    (dB)

    Center Frequency (MHz))

    SAF

    (dB)

    Center Frequency (MHz))

    SAF

    (dB)

    1164

    -67.4

    1177

    -66.3

    1190

    -18.3

    1203

    -1.2

    1165

    -67.5

    1178

    -64.7

    1191

    -18.5

    1204

    -3.9

    1166

    -68.5

    1179

    -63.2

    1192

    -18.2

    1205

    -6.8

    1167

    -69.4

    1180

    -62.4

    1193

    -16.3

    1206

    -8.7

    1168

    -70.0

    1181

    -62.2

    1194

    -13.3

    1207

    -11.3

    1169

    -68.7

    1182

    -62.8

    1195

    -10.6

    1208

    -14.0

    1170

    -67.2

    1183

    -63.6

    1196

    -8.2

    1209

    -17.1

    1171

    -65.8

    1184

    -61.8

    1197

    -6.2

    1210

    -18.3

    1172

    -65.3

    1185

    -52.6

    1198

    -3.1

    1211

    -18.4

    1173

    -65.2

    1186

    -42.2

    1199

    -0.8

    1212

    -17.7

    1174

    -66.0

    1187

    -32.0

    1200

    0.0

    1213

    -18.8

    1175

    -66.9

    1188

    -22.8

    1201

    0.0

    1214

    -20.7

    1176

    -67.5

    1189

    -19.5

    1202

    -0.1

    1215

    -27.6

    III-9 Results of the epfd calculation for GLONASS-M in the worst 1 MHz of the 1164-1215 MHz band.

    See Attachment 4

    Additional simulation data for non-GSO systems only:

    :

    Time step (sec)

    30

    Number of time steps

    22977

    Technical Contact Person

    Name:

    Igor Zheltonogov

    Tel./Fax:

    +7 095 2300085 / +7 095 2300085

    E-mail Address:[email protected]

    IVCOMPASS-M

    IV-1RNSS ITU publication reference

    RNSS network name

    BR Network ID

    ITU Publication reference

    IFIC

    COMPASS

    COMPASS-M

    API/A/1304

    2420

    COMPASS

    COMPASS-MG

    API/A/2997

    2512

    IV-2COMPASS-M satellite system constellation parameters

    N = 30: number of space stations of the non-GSO system

    K = 6:number of orbital planes

    h = 20200:satellite altitude above the Earth (km)

    I = 55:inclination angle of the orbital plane above the Equator (degrees).

    Satellite indexI

    RAAN(i,0 (degrees)

    Argument of latitude ui,0 (degrees)

    1

    0.00000

    0.00000

    2

    0.00000

    72.00000

    3

    0.00000

    144.00000

    4

    0.00000

    216.00000

    5

    0.00000

    288.00000

    6

    60.00000

    12.00000

    7

    60.00000

    84.00000

    8

    60.00000

    156.00000

    9

    60.00000

    228.00000

    10

    60.00000

    300.00000

    11

    120.00000

    24.00000

    12

    120.00000

    96.00000

    13

    120.00000

    168.00000

    14

    120.00000

    240.00000

    15

    120.00000

    312.00000

    16

    180.00000

    36.00000

    17

    180.00000

    108.00000

    18

    180.00000

    180.00000

    19

    180.00000

    252.00000

    20

    180.00000

    324.00000

    21

    240.00000

    48.00000

    22

    240.00000

    120.00000

    23

    240.00000

    192.00000

    24

    240.00000

    264.00000

    25

    240.00000

    336.00000

    26

    300.00000

    60.00000

    27

    300.00000

    132.00000

    28

    300.00000

    204.00000

    29

    300.00000

    276.00000

    30

    300.00000

    348.00000

    IV-4Maximum COMPASS-M space station pfd versus the elevation angle at 40000 feet above the Earths surface (worst 1 MHz)

    Elevation angle (each 1)

    Pfd(dB(W/(m2/MHz)))

    4

    -139.975

    3

    -139.937

    -2

    -139.900

    -1

    -139.862

    0

    -139.825

    1

    -139.787

    2

    -139.750

    3

    -139.713

    4

    -139.675

    5

    -139.638

    6

    -139.601

    7

    -139.563

    8

    -139.526

    9

    -139.489

    10

    -139.452

    11

    -139.415

    12

    -139.379

    13

    -139.342

    14

    -139.306

    15

    -139.270

    16

    -139.234

    17

    -139.198

    18

    -139.162

    19

    -139.127

    20

    -139.091

    21

    -139.057

    22

    -139.022

    23

    -138.987

    24

    -138.953

    25

    -138.919

    26

    -138.886

    27

    -138.852

    28

    -138.819

    29

    -138.786

    30

    -138.754

    31

    -138.722

    32

    -138.690

    33

    -138.659

    34

    -138.628

    35

    -138.598

    36

    -138.567

    37

    -138.538

    38

    -138.508

    39

    -138.479

    40

    -138.451

    41

    -138.422

    42

    -138.395

    43

    -138.367

    44

    -138.341

    45

    -138.314

    46

    -138.288

    47

    -138.263

    48

    -138.238

    49

    -138.214

    50

    -138.190

    51

    -138.166

    52

    -138.144

    53

    -138.121

    54

    -138.099

    55

    -138.078

    56

    -138.057

    57

    -138.037

    58

    -138.017

    59

    -137.998

    60

    -137.979

    61

    -137.961

    62

    -137.944

    63

    -137.927

    64

    -137.911

    65

    -137.895

    66

    -137.880

    67

    -137.865

    68

    -137.851

    69

    -137.838

    70

    -137.825

    71

    -137.813

    72

    -137.801

    73

    -137.790

    74

    -137.780

    75

    -137.770

    76

    -137.761

    77

    -137.753

    78

    -137.745

    79

    -137.737

    80

    -137.731

    81

    -137.725

    82

    -137.719

    83

    -137.715

    84

    -137.711

    85

    -137.707

    86

    -137.704

    87

    -137.702

    88

    -137.700

    89

    -137.699

    90

    -137.699

    IV-8COMPASS-M satellite system spectrum

    The level of spectrum emission in each 1 MHz relative to the spectrum value at the worst 1MHz of the whole band (1164-1215MHz) is provided below as the Spectral Adjustment Factor (SAF) in dB.

    Normalised Signal Power Spectrum

    Center Frequency(MHz)

    SAF(dB)

    Center Frequency(MHz)

    SAF(dB)

    Center Frequency(MHz)

    SAF(dB)

    Center Frequency(MHz)

    SAF(dB)

    1164

    -132.5

    1177

    -87.0

    1190

    -48.5

    1203

    -0.6

    1165

    -129.0

    1178

    -83.5

    1191

    -48.5

    1204

    -0.16

    1166

    -125.5

    1179

    -80.0

    1192

    -48.5

    1205

    0

    1167

    -122.0

    1180

    -76.5

    1193

    -48.5

    1206

    -0.16

    1168

    -118.5

    1181

    -73.0

    1194

    -48.5

    1207

    -0.6

    1169

    -115.0

    1182

    -69.5

    1195

    -30.0

    1208

    -1.3

    1170

    -111.5

    1183

    -66.0

    1196

    -18.0

    1209

    -2.4

    1171

    -108.0

    1184

    -62.5

    1197

    -12.0

    1210

    -3.8

    1172

    -104.5

    1185

    -59.0

    1198

    -8.2

    1211

    -5.7

    1173

    -101.0

    1186

    -55.5

    1199

    -5.7

    1212

    -8.2

    1174

    -97.5

    1187

    -52.0

    1200

    -3.8

    1213

    -12.0

    1175

    -94.0

    1188

    -48.5

    1201

    -2.4

    1214

    -18.0

    1176

    -90.5

    1189

    -48.5

    1202

    -1.3

    1215

    -30.0

    IV-9 Results of the epfd calculation for COMPASS-M in the worst 1 MHz of the 1164-1215MHz band

    See Attachment 4

    Additional simulation data for non-GSO systems only:

    Time step (sec)

    30

    Number of time steps

    2882

    Technical Contact Person

    Name: ZhaoXiaodong

    Senior Engineer of Beijing Global Information Center of Application and Exploitation

    Tel./Fax:

    Tel: 86-10-62477702

    Fax: 86-10-62477702

    E-mail Address: [email protected]

    VN-SAT-HEO2

    V-1RNSS ITU publication reference

    RNSS network name

    BR Network ID

    ITU Publication reference

    IFIC

    N-SAT-HEO2

    102540591

    API/A/2471 MOD-1

    2490

    V-2N-SAT-HEO2 satellite system constellation parameters

    N (number of space stations of the non-GSO system) : 3

    K(number of orbital planes): 3

    h(satellite altitude above the Earth at apogee): 39,970 km

    hP(satellite altitude above the Earth at perigee): 31,602 km

    I(inclination angle of the orbital plane above the Equator) : 45 degrees

    Satellite indexI

    RAAN(i,0 (degrees)

    Argument of latitude ui,0 (degrees)

    Argument of perigee of the non-GSO system

    (:

    1

    206.97

    294.43

    270 degrees

    2

    326.97

    159.16

    270 degrees

    3

    86.97

    56.67

    270 degrees

    V-6Maximum N-SAT-HEO2 space station off-axis EIRP density and additional satellite antenna pointing information (worst 1MHz)

    a) Satellite antenna pointing direction and other operational information to be used in calculating epfd values.

    (1) When the satellite is north of latitude 26.5N, the boresight of the antenna points to a fixed location on the Earths surface corresponding to latitude of 34.67N/ longitude of 135E.

    (2) When the satellite is south of