Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20070622-00085 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2007062200085_575646

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: ECHOSTAR-11 12/15/2007 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/1/2005 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 5/30/2007 32 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: 10/1/2007 11/15/2007 768 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 Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode f. 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) 17300 M 17800 M R Feeder Link for Broadcasting Satellite Service in FSS 12200 M 12700 M T Broadcasting Satellite Service - Video 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: 110 W Consistent with Region 2 USA Plan and existing Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be EchoStar license. N/S Station-Keeping provided (Optional): d. Toward West: Degrees E/W 0.05 Degrees Tolerance: g. Westernmost: 110 W e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: 110 W i. Reason for service are selection (Optional): Cluster range of Region 2 BSS Plan for the 110W nominal orbital slot is from 110.2W to 109.8W.

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 (o) Other Plane (Seconds) Node (Deg.) (Degrees) Angle 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) CONUS+ S CONUS, Alaska, Hawaii, Puerto Rico CHEYENNE S Area around Cheyenne, WY GILBERT S Area around Gilbert, AZ GLOBAL S Visible Earth

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) (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Input Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) Losses Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) (db/K) (dBW/m2) TRH T 35.7 22.5 0.12 0.2 30 N CONUS+ 4.3 112.2 56.2 TLH T 35.7 22.5 0.12 0.2 28.8 N CONUS+ 4.3 112.2 56.2 TRS T 35.7 22.9 0.12 0.2 30 N CONUS+ 3.4 204.2 58.8 TLS T 35.7 22.9 0.12 0.2 28.8 N CONUS+ 3.4 204.2 58.8 OMN R 3 -4 1 1 30 N GLOBAL 10000 -37 -83 OMN T 3 -4 1 1 30 N GLOBAL 3.6 15.1 14.8 TCO R 44.9 38 0.12 0.2 30 N CHEYENN 32000 -3.1 -93 TMO T 35.7 29.7 0.12 0.2 28.8 N CONUS+ 10 0.014 17.2 TCO R 44.6 38 0.12 0.2 30 N GILBERT 32000 -3.4 -93 RR1 R 44.9 41.9 0.12 0.2 30 N CHEYENN 5358 7.6 -100.4 21 1 RL1 R 44.9 41.9 0.12 0.2 30 N CHEYENN 5358 7.6 -100.4 21 1 RR2 R 44.6 41.6 0.12 0.2 30 N GILBERT 6124 6.7 -99.5 21 1 RL2 R 44.6 41.6 0.12 0.2 30 N GILBERT 6124 6.7 -99.5 21 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) TRH T C -110 TRH.gxt TLH T C -110 TLH.gxt TRS T C -110 TRS.gxt TLS T C -110 TLS.gxt TCO R C -110 TCOS1.gxt TCO R C -110 TCOS2.gxt TMO T C -110 TMOS.gxt RR1 R C -110 RR1.gxt RL1 R C -110 RL1.gxt RR2 R C -110 RR2.gxt RL2 R C -110 RL2.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 ID Gain (dB) No. ID No. (T or C) R01 24000 R 17324 R C H01 122.3 R01 RR1 T01 TRH R03 24000 R 17353.16 R C H03 122.3 R03 RR1 T03 TRH R05 24000 R 17382.32 R C H05 122.3 R05 RR1 T05 TRH R07 24000 R 17411.48 R C H07 122.3 R07 RR1 T07 TRH R09 24000 R 17440.64 R C H09 122.3 R09 RR1 T09 TRH R11 24000 R 17469.8 R C H11 122.3 R11 RR1 T11 TRH R13 24000 R 17498.96 R C H13 122.3 R13 RR1 T13 TRH R15 24000 R 17528.12 R C H15 122.3 R15 RR1 T15 TRH R17 24000 R 17557.28 R C H17 122.3 R17 RR1 T17 TRH R19 24000 R 17586.44 R C H19 122.3 R19 RR1 T19 TRH R21 24000 R 17615.6 R C H21 122.3 R21 RR1 T21 TRH R23 24000 R 17644.76 R C H23 122.3 R23 RR1 T23 TRH R25 24000 R 17673.92 R C H25 122.3 R25 RR1 T25 TRH R27 24000 R 17703.08 R C H27 122.3 R27 RR1 T27 TRH R29 24000 R 17732.24 R C H29 122.3 R29 RR1 T29 TRH R31 24000 R 17761.4 R C H31 122.3 R31 RR1 T31 TRH R02 24000 R 17338.58 L C H02 122.3 R02 RL1 T02 TLH R04 24000 R 17367.74 L C H04 122.3 R04 RL1 T04 TLH R06 24000 R 17396.9 L C H06 122.3 R06 RL1 T06 TLH R08 24000 R 17426.06 L C H08 122.3 R08 RL1 T08 TLH R10 24000 R 17455.22 L C H10 122.3 R10 RL1 T10 TLH R12 24000 R 17484.38 L C H12 122.3 R12 RL1 T12 TLH R14 24000 R 17513.54 L C H14 122.3 R14 RL1 T14 TLH R16 24000 R 17542.7 L C H16 122.3 R16 RL1 T16 TLH R18 24000 R 17571.86 L C H18 122.3 R18 RL1 T18 TLH R20 24000 R 17601.02 L C H20 122.3 R20 RL1 T20 TLH R22 24000 R 17630.18 L C H22 122.3 R22 RL1 T22 TLH R24 24000 R 17659.34 L C H24 122.3 R24 RL1 T24 TLH R26 24000 R 17688.5 L C H26 122.3 R26 RL1 T26 TLH R28 24000 R 17717.66 L C H28 122.3 R28 RL1 T28 TLH

R30 24000 R 17746.82 L C H30 122.3 R30 RL1 T30 TLH R32 24000 R 17775.98 L C H32 122.3 R32 RL1 T32 TLH T01 24000 T 12224 R C S01 124.9 R01 RR1 T01 TRS T03 24000 T 12253.16 R C S03 124.9 R03 RR1 T03 TRS T05 24000 T 12282.32 R C S05 124.9 R05 RR1 T05 TRS T07 24000 T 12311.48 R C S07 124.9 R07 RR1 T07 TRS T09 24000 T 12340.64 R C S09 124.9 R09 RR1 T09 TRS T11 24000 T 12369.8 R C S11 124.9 R11 RR1 T11 TRS T13 24000 T 12398.96 R C S13 124.9 R13 RR1 T13 TRS T15 24000 T 12428.12 R C S15 124.9 R15 RR1 T15 TRS T17 24000 T 12457.28 R C S17 124.9 R17 RR1 T17 TRS T19 24000 T 12486.44 R C S19 124.9 R19 RR1 T19 TRS T21 24000 T 12515.6 R C S21 124.9 R21 RR1 T21 TRS T23 24000 T 12544.76 R C S23 124.9 R23 RR1 T23 TRS T25 24000 T 12573.92 R C S25 124.9 R25 RR1 T25 TRS T27 24000 T 12603.08 R C S27 124.9 R27 RR1 T27 TRS T29 24000 T 12632.24 R C S29 124.9 R29 RR1 T29 TRS T31 24000 T 12661.4 R C S31 124.9 R31 RR1 T31 TRS T02 24000 T 12238.58 L C S02 124.9 R02 RL1 T02 TLS T04 24000 T 12267.74 L C S04 124.9 R04 RL1 T04 TLS T06 24000 T 12296.90 L C S06 124.9 R06 RL1 T06 TLS T08 24000 T 12326.06 L C S08 124.9 R08 RL1 T08 TLS T10 24000 T 12355.22 L C S10 124.9 R10 RL1 T10 TLS T12 24000 T 12384.38 L C S12 124.9 R12 RL1 T12 TLS T14 24000 T 12413.54 L C S14 124.9 R14 RL1 T14 TLS T16 24000 T 12442.7 L C S16 124.9 R16 RL1 T16 TLS T18 24000 T 12471.86 L C S18 124.9 R18 RL1 T18 TLS T20 24000 T 12501.02 L C S20 124.9 R20 RL1 T20 TLS T22 24000 T 12530.18 L C S22 124.9 R22 RL1 T22 TLS T24 24000 T 12559.34 L C S24 124.9 R24 RL1 T24 TLS T26 24000 T 12588.5 L C S26 124.9 R26 RL1 T26 TLS T28 24000 T 12617.66 L C S28 124.9 R28 RL1 T28 TLS T30 24000 T 12646.82 L C S30 124.9 R30 RL1 T30 TLS T32 24000 T 12675.98 L C S32 124.9 R32 RL1 T32 TLS CMD1 1000 R 17794 R T CMDA CMD1 OMNR CMD2 1000 R 17797 R T CMDB CMD2 OMNR TLM1 1000 T 12692 R T CMDC CMD1 TCOS1 TLM2 1000 T 12693 R T CMDD CMD1 TCOS2 TLM3 1000 T 12208 L T CMDE CMD2 TCOS1

CMDF CMD2 TCOS2 TLMA TLM1 OMNT TLMB TLM2 OMNT TLMC TLM1 TMOS TLMD TLM2 TMOS TLME TLM3 TMOS H33 121.7 R01 RR2 T01 TRH H35 121.7 R03 RR2 T03 TRH H37 121.7 R05 RR2 T05 TRH H39 121.7 R07 RR2 T07 TRH H41 121.7 R09 RR2 T09 TRH H43 121.7 R11 RR2 T11 TRH H45 121.7 R13 RR2 T13 TRH H47 121.7 R15 RR2 T15 TRH H49 121.7 R17 RR2 T17 TRH H51 121.7 R19 RR2 T19 TRH H53 121.7 R21 RR2 T21 TRH H55 121.7 R23 RR2 T23 TRH H57 121.7 R25 RR2 T25 TRH H59 121.7 R27 RR2 T27 TRH H61 121.7 R29 RR2 T29 TRH H63 121.7 R31 RR2 T31 TRH H34 121.7 R02 RL2 T02 TLH H36 121.7 R04 RL2 T04 TLH H38 121.7 R06 RL2 T06 TLH H40 121.7 R08 RL2 T08 TLH H42 121.7 R10 RL2 T10 TLH H44 121.7 R12 RL2 T12 TLH H46 121.7 R14 RL2 T14 TLH H48 121.7 R16 RL2 T16 TLH H50 121.7 R18 RL2 T18 TLH H52 121.7 R20 RL2 T20 TLH H54 121.7 R22 RL2 T22 TLH H56 121.7 R24 RL2 T24 TLH H58 121.7 R26 RL2 T26 TLH H60 121.7 R28 RL2 T28 TLH H62 121.7 R30 RL2 T30 TLH H64 121.7 R32 RL2 T32 TLH S33 124.3 R01 RR2 T01 TRS

S35 124.3 R03 RR2 T03 TRS S37 124.3 R05 RR2 T05 TRS S39 124.3 R07 RR2 T07 TRS S41 124.3 R09 RR2 T09 TRS S43 124.3 R11 RR2 T11 TRS S45 124.3 R13 RR2 T13 TRS S47 124.3 R15 RR2 T15 TRS S49 124.3 R17 RR2 T17 TRS S51 124.3 R19 RR2 T19 TRS S53 124.3 R21 RR2 T21 TRS S55 124.3 R23 RR2 T23 TRS S57 124.3 R25 RR2 T25 TRS S59 124.3 R27 RR2 T27 TRS S61 124.3 R29 RR2 T29 TRS S63 124.3 R31 RR2 T31 TRS S34 124.3 R02 RL2 T02 TLS S36 124.3 R04 RL2 T04 TLS S38 124.3 R06 RL2 T06 TLS S40 124.3 R08 RL2 T08 TLS S42 124.3 R10 RL2 T10 TLS S44 124.3 R12 RL2 T12 TLS S46 124.3 R14 RL2 T14 TLS S48 124.3 R16 RL2 T16 TLS S50 124.3 R18 RL2 T18 TLS S52 124.3 R20 RL2 T20 TLS S54 124.3 R22 RL2 T22 TLS S56 124.3 R24 RL2 T24 TLS S58 124.3 R26 RL2 T26 TLS S60 124.3 R28 RL2 T28 TLS S62 124.3 R30 RL2 T30 TLS S64 124.3 R32 RL2 T32 TLS

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) QPSK1 24M0G7W 24000 4 27647 0.6912 0 5.7 28 QPSK2 24M0G7W 24000 4 30719 0.768 0 6.6 28 8PSK1 25M8G7W 25800 8 41200 0.6389 0 7.5 28

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) CMD 1M00F2D 1000 1 10 22.2 TLM 1M00G2D 1000 1 9 21.2

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. (o)Assoc. Transponder (kHz) No.) Bandwidth (Table (Table S12) Stn. Max. Power (dBW) Power Flux Stn (a) Start (b) End (kHz) S11) Antenna Density Rec. G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dBW/m2/Hz) (dB/K) H01 H64 QPSK1 1 E-11 Link Budg 65.7 4.1 16.1 43 56.2 13.2 H01 H64 QPSK2 1 E-11 Link Budg 65.7 4.1 16.1 43 56.2 13.2 H01 H64 8PSK1 1 E-11 Link Budg 65.7 4.1 16.1 43 56.2 13.2 S01 S64 QPSK1 1 E-11 Link Budg 65.7 4.1 16.1 46 58.8 13.2 S01 S64 QPSK2 1 E-11 Link Budg 65.7 4.1 16.1 46 58.8 13.2 S01 S64 8PSK1 1 E-11 Link Budg 65.7 4.1 16.1 46 58.8 13.2 CMDA CMDB CMD 1 E-11 Link Budg 63.9 16.4 36.4 -37 CMDC CMDF CMD 1 E-11 Link Budg 63.9 2.9 8.9 -3 TLMA TLMB TLM 1 E-11 Link Budg 7.8 14.8 48 TLMC TLME TLM 1 E-11 Link Budg 11.2 17.2 48

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: 530 Echostar Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Cheyenne Laramie WY 82007 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 307-633-5460 Remote Control (TT C) Location(s): S14a: Street Address: 801 North Dish Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Gilbert Maricopa AZ 85233 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 480-558-2778

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 2479 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3146 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5619 6.9 0.8377 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1030 8 0.8635 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 92 32.5 0.7234 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): 14102 14102 14102 14102 Bus (Watts): (b): (g): (l): (q): 3461 1705 3461 1705 Total (Watts): (c): (h): (m): (r): 17563 15807 17563 15807 Solar Array (Watts): (d): (i): (n): (s): 19493 17522 18478 16610 Depth of Battery (e) (j) (o) (t) Discharge (%): 76.5 % 76.5 % 76.5 % 76.5 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO X 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: 2007-06-29 12:02:17
Document Modified: 2007-06-29 12:02:17
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