Designation | 28134 / 03060A |
Launch date | 28 Dec 2003 |
Country of origin | CIS |
Mission | Telecommunications |
Geostationary orbit | Express-05, 53°E |
Launch vehicle | Proton #305 |
Begin | End | Position |
L: 28 Dec 2003 | Jul 2015 | Express-05, 53°E |
Aug 2015 | Mar 2017 | Express-06, 80°E |
Mar 2017 | Jan 2019 | Express-06, 80°E, inclined |
Out of service | Jan 2019 |
Cause | Sent to Junk orbit |
Prime contractor | NPO PM (bus only) |
Platform | Express-727M |
Mass at launch | 2600 kg |
Payload mass | 590 kg |
Dimension | |
Solar array | |
Stabilization | 3-axis |
DC power | 6000 W |
Design lifetime | 12 years |
Main transponders | 24 |
Backup transponders | 8 |
Power | 103.5 W |
Bandwidth | 54 MHz |
Coverage & EIRP max |
fixed
beam: Europe: triangle formed by Spain, Irak and European part of Russia wide fixed beam: Europe, most of the Middle East, Central Asia, 2/3 of Russia steerable 1 (4° x 4°) steetable 2 (3.5° x 7°) |
EIRP max |
fixed
beam: Europe: 50 dBW wide fixed beam: 48 dBW steerable 1: 52 dBW steetable 2: 50 dBW |
G/T max |
fixed
beam: Europe: +6 dB/K wide fixed beam: +4 dB/K steerable 1: +8 dB/K steetable 2: +5 dB/K |
Polarization | linear H/V cross-pol |
Horizontal Uplink |
Horizontal Downlink | Transponder |
Vertical Downlink |
Vertical Uplink |
10.98125 | B1 | 14.28125 | ||
14.28125 | B2 | 10.98125 | ||
11.04375 | B3 | 14.34375 | ||
14.34375 | B4 | 11.04375 | ||
11.10625 | B5 | 14.40625 | ||
14.40625 | B6 | 11.10625 | ||
11.16875 | B7 | 14.46875 | ||
14.46875 | B8 | 11.16875 | ||
14.03125 | D1 | 11.48125 | ||
11.48125 | D2 | 14.03125 | ||
14.09375 | D3 | 11.54375 | ||
11.54375 | D4 | 14.09375 | ||
14.15625 | D5 | 11.60625 | ||
11.60625 | D6 | 14.15625 | ||
14.21875 | D7 | 11.66875 | ||
11.66875 | D8 | 14.21875 | ||
13.78125 | A1 | 12.53125 | ||
12.53125 | A2 | 13.78125 | ||
13.84375 | A3 | 12.59375 | ||
12.59375 | A4 | 13.84375 | ||
13.90625 | A5 | 12.59375 | ||
12.59375 | A6 | 13.90625 | ||
13.96875 | A7 | 12.71875 | ||
12.71875 | A8 | 13.96875 |