Hylas 1
Cost EUR 120 million (EUR 34 million are paid by ESA). Launch initially planned
in 2008.
The original launch contract on
Falcon
9 contained options for 1 to 3 other launches. In Jul 2009, the company decided
to move to
Ariane
in order to secure a launch date in Q2 2010. That move would cost $70
million.
Started service in April 2011.
Begin
|
End
|
Position
|
L:
26 Nov 2010
|
Feb
2011
|
31°E
|
Mar
2011
|
Jan
2019
|
33.5°W
|
Feb
2019
|
May
2019
|
13.8°E
|
Jun
2019
|
Sep
2019
|
18.2°W
|
Oct
2019
|
Mar
2020
|
79°W
|
Jun
2020
|
Sep
2020
|
160°E
|
Sep
2020
|
Dec
2020
|
156°E
inclined
|
Jan
2021
|
Apr
2021
|
117.2°E
inclined
|
May
2021
|
Aug
2021
|
158.7°E
inclined
|
Dec
2021
|
Mar
2022
|
80.8°W
inclined
|
Mar
2022
|
Jun
2022
|
123.2°W
inclined
|
Jul
2022
|
Oct
2022
|
79°W
inclined
|
Nov
2022
|
Feb
2023
|
51.75°E
inclined
|
Mar
2023
|
Jun
2023
|
13.8°E
inclined
|
Aug
2023
|
Nov
2023
|
159°E
inclined
|
Nov
2023
|
Feb
2024
|
156°E
inclined
|
|
|
moving
West
|
http://www.avantiplc.com/
http://www.avanti-communications.com/
sat-index articles
Lyngsat
transponder loading
Prime
contractor
|
EADS
Astrium
|
Platform
|
ISRO
I2K
|
Mass
at launch
|
2570
kg
|
Dry
mass
|
1125
kg
|
Dimension
|
2.5
x 1.6 x 1.5 m
|
Solar
array
|
9
m span?
|
Stabilization
|
3-axis
|
DC
power
|
EOL:
3.2 kW
|
Design
lifetime
|
15
years
|
First contract for EADS's Generic Flexible Payload and Next Generation
Antenna.
Main
transponders
|
2 |
Backup
transponders
|
|
Power
|
|
Bandwidth
|
|
Coverage
|
Western
and Central Europe
|
EIRP
max
|
|
G/T
max
|
|
Polarization
|
|
Main
transponders
|
6 |
Backup
transponders
|
|
Power
|
|
Bandwidth
|
|
Coverage
|
8
spot beams
|
EIRP
max
|
|
Polarization
|
circular
|
Frequencies
|
Uplink:
Downlink:
|