Astra 2B
The launch of the satellite was delayed by problems experienced by
manufacturers with faulty solar arrays and leaking thrusters.
Begin
|
End
|
Position
|
L:
14 Sep 2000
|
Oct
2000
|
33.5°E
|
Nov
2000
|
Feb
2013
|
28.2°E
|
Feb
2013
|
Jan
2014
|
19.2°E
|
Feb
2014
|
Oct
2014
|
31.3°E
|
Oct
2014
|
Jul
2016
|
31.3°E,
inclined
|
Aug
2016
|
Nov
2016
|
39°E,
inclined
|
Dec
2016
|
May
2017
|
19.4°E,
inclined
|
Aug
2017
|
Apr
2018
|
19.6°W,
inclined
|
Jun
2018
|
May
2021
|
19.5°E,
inclined
|
Out
of service
|
Jun
2021
|
Cause
|
Sent
to the junk orbit
|
sat-index articles
Lyngsat
transponder loading
Northern beam
Southern beam
Prime
contractor
|
Matra
Marconi Space
|
Platform
|
Eurostar-2000+
(#18)
|
Mass
at launch
|
3315
kg
|
Dry
mass
|
1400
kg
|
Dimension
|
|
Solar
array
|
|
Stabilization
|
3-axis
|
DC
power
|
|
Design
lifetime
|
15
years
|
Main
transponders
|
28
(30 for the first 5 years)
|
Backup
transponders
|
|
Power
|
108
W
|
Bandwidth
|
33
MHz
|
Coverage
|
same
as
Astra 2A
|
EIRP
max
|
52
dBW
|
Polarization
|
linear
H/V
|
Frequencies
|
band E
&
band F
|
Main
transponders
|
16
|
Backup
transponders
|
|
Power
|
|
Bandwidth
|
|
Coverage
|
mobile
beam: Western Africa
|
EIRP
max
|
|
Polarization
|
linear
H/V
|
Frequencies
|
band G
|