Spacecraft n°: |
Russia satellite n°: |
Launch data:
| Designation | 28909 / 05048B |
| Launch date | 21 Dec 2005 - 19:34 UT |
| Launch site | Pl, LC-132/1 |
| Launch vehicle |
Cosmos-3M (11K65M s/n: 232) |
| Mission | Commercial: Communication, Store-Dump |
| Intermediate LEO Earth orbit on Dec 22.12: |
| Perigee / Apogee | 1438 x 1448 km |
| Eccentricity | 6,40E-04 |
| Inclination | 82.47° |
| Period | 114.73 min |
|
|
Spacecraft data:
| Prime contractor | NPO Prikladnoy Mekhaniki (NPO-PM) |
| Operator | RKA |
| Platform | |
| Mass at launch | 280 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | 40 W |
| Design lifetime | 5 yrs, still in orbit |
|
Decay:
| Out of service: | Dec 2011 |
| Cause: | |
|
Descriptions:
Gonets-D1M are upgraded versions of the Gonets-D1
satellites, a civilian derivate of the military Strela-3
satellite system. The Gonets system was offered to support international health
organizations to meet their global communications needs for the transfer of
medical data and records to remote sites.
After two prototype Gonets-D
satellites the operational Gonets-D1 was to be deployed in a constellation of 12
satellites consisting of 6 satellites in 2 orbital planes between 1996 and 1998.
Each satellite had a single simultaneous earth-space and space-earth channel.
On-board storage was 12 Mbits of data, with a transmission rate of 2.4 kbit/sec.
Attitude control was achieved through gravity-gradient stabilization. The
electrical power system, provided by solar cells and nickel-hydrogen batteries,
provided an average 40 W for the payload which was designed to operate for five
years.
In the commercial variant, the satellites, known as Gonets (Messenger), were
capable of store-dump communications on 2-3 channels in the 2004-400 MHz band
with a transmitter output power of 10 W. Data transmission rates available
include 2.4 kbits/s, 9.6 kbit/s, and 64 kbit/s with an onboard storage capacity
of 8 Mbytes. A handheld user terminal (UT-P) resembles a cellular phone and
weighs only 1-3 kg. Finally the 250 kg Gonets were to be deployed at 1,350 km at
82.5 degrees, similar to the Strela-3
satellites, but distributed among six orbital planes for a total constellation
of 36 spacecraft. This infrastructure would ensure a mean communication waiting
time of less than 20 minutes with more than 80% probability.
Ref.: #7, #14, #206, #207, #226 - update: 02.08.12