Payload:
Telstar 14R/Estrela do Sul 2
SS/L 1300
Separated spacecraft mass: ~5,000 kg
Launch Vehicle:
Proton M/Breeze M
705,000 kg (1,554,000 lbs), including payload
58.2 m (191 ft)
Launch Date:
21 May 2011, Baikonur
Launch Time:
01:15 Baikonur
19:15 GMT, 20 May
15:15 EDT, 20 May
Launch Site:
Baikonur Cosmodrome, Kazakhstan
Launch Pad 39
Launch Customer:
Telesat, Ontario, Canada
Satellite Manufacturer:
Space Systems/Loral, California, USA
Launch Vehicle Manufacturer:
Khrunichev State Research and Production Space Center,
Moscow, Russia
Launch Services Provider:
International Launch Services, Virginia, USA
Satellite Use:
Telstar 14R/Estrela do Sul 2 is a commercial communications satellite built by Space Systems/Loral for Telesat. The satellite will utilize 46 high powered Ku-band transponders (58 36-MHz transponder equivalents) over five coverage beams consisting of: Brazil, the Continental United States (including the Gulf of Mexico and northern Caribbean), the Southern Cone of South America, the Andean region (including Central America and southern Caribbean), and the North and Mid-Atlantic Ocean. Following its launch, Telstar 14R/Estrela do Sul 2 will be located at 63 degrees west longitude where it will replace and augment the communications capability currently supplied by Telesat’s Telstar 14/ Estrela do Sul.
Satellite Statistics:
__ Ku-band capacity
__ 46 high powered Ku-band transponders (58 36-MHz transponder equivalents)
__ Anticipated service life: 15 years
Mission Profile:
The Proton M launch vehicle, utilizing a 5-burn Breeze M mission design, will lift off from Pad 39 at Baikonur Cosmodrome, Kazakhstan, with the Telstar 14R/Estrela do Sul satellite on board. The first three stages of the Proton will use a standard ascent profile to place the orbital unit (Breeze M upper stage and the satellite) into a sub-orbital trajectory. From this point in the mission, the Breeze M will perform planned mission maneuvers to advance the orbital unit first to a circular parking orbit, then to an intermediate orbit, followed by a transfer orbit, and finally to a geosynchronous transfer orbit. Separation of the satellite is scheduled to occur approximately 9 hours, 13 minutes after liftoff.
Target Orbit at Separation:
Apogee: 35,786 km (22,236 miles)
Perigee: 8,850 km (5,499 miles)
Inclination: 13.8 degrees
Spacecraft Separation:
Approximately 9 hours, 13 minutes after liftoff
ILS Mission Statistics:
__7th Telesat Satellite Launched on ILS Proton
__17th Space Systems/Loral Satellite Launched on ILS Proton
__1st ILS Proton Launch in 2011
__65th ILS Proton Launch Overall; 364th Proton mission since 1965
More Information:
General mission information and launch status updates are available at the ILS website or on the ILS U.S. domestic Launch Hotline at 1-800-852-4980.
Live Broadcast Details:
Live Coverage starting at 14:45 EDT
Launch is scheduled for 15:15:19 EDT
Launch Broadcast concludes no later than 15:45 EDT
Anik F2 satellite time from IMG/Washington, DC will start at 14:15 EDT for test signal
AMC-3 satellite time from IMG/Washington, DC will start at 14:15 EDT for test signal
European test signals from IMG/Washington, DC will start at 14:15 EDT for test signal
Baikonur to U.S. signal starts at 13:45 Eastern for test signal
Webcast: http://telstar14r.imgondemand.com/
In North America, the Launch Broadcast will be Seen on the Following:
AMC3 C04 (36 MHz)
87 degrees west longitude
U/L Frequency: 6005.0 Horizontal
D/L Frequency: 3780.0 Vertical
Audio: channel 1 and 2
In Canada, the Launch Broadcast will be Seen on the Following:
Anik F2C 3B
36 mhz.
U/L Frequency: 6045.0 Horizontal
D/L Frequency: 3820.0 Vertical
Audio: 6.2 and 6.8
In Europe, the Launch Broadcast will be Seen on the Following:
Eutelsat W2A, B1 (V/H) #5-20275
Channel: CH-3Upper
U/L Frequency: 14,314.00 Vertical
D/L Frequency: 11,014.00 Horizontal
625 PAL
9 Mhz
Audio: 2 channels
Symbol rate: 5.632
FEC: 3/4
MPEG: 4:2:0 MPEG2
Media Inquiries:
Karen Monaghan, Director of Communications, International Launch Services, Reston, Va.; +1-571-633-7549; mobile: +1-571-282-5195; k.monaghan@ilslaunch.com, Visit the ILS website at www.ilslaunch.com.