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Atlas V 551 | ViaSat-3 F2 (ViaSat-3 EMEA)
United Launch AllianceLaunch Successful

ViaSat-3 F2 (ViaSat-3 EMEA)

Atlas V 551

Historical mission record

This page records Atlas V 551 | ViaSat-3 F2 (ViaSat-3 EMEA) and its reported outcome: Launch Successful. The date above is a historical record.

Source record updated . This is a source update, not a confirmed launch time.

Check the source: Atlas V ViaSat-3 F2 ↗ · Launch Library ↗ · Flight Club ↗

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Launch success with satellite in contact.

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Mission status
Launch Successful

Status reported by the mission data provider.

LAUNCH SITECape Canaveral SFS, FL, USA

Mission

The ViaSat-3 is a series of three Ka-band satellites is expected to provide vastly superior capabilities in terms of service speed and flexibility for a satellite platform. Each ViaSat-3 class satellite is expected to deliver more than 1-Terabit per second of network capacity, and to leverage high levels of flexibility to dynamically direct capacity to where customers are located.

Launch vehicle
Atlas V 551
Mission type
Communications
Destination orbit
Geostationary Transfer Orbit
Launch pad
Space Launch Complex 41
Provider
United Launch Alliance

The vehicle

Published configuration and flight history.

Atlas V 551
Launch vehicle

Atlas V 551

Atlas V is an expendable launch system in the Atlas rocket family. It was formerly operated by Lockheed Martin and is now operated by United Launch Alliance (ULA), a joint venture with Boeing. Each Atlas V rocket uses a Russian-built RD-180 engine burning kerosene and liquid oxygen to power its first stage and an American-built RL10 engine burning liquid hydrogen and liquid oxygen to power its Centaur upper stage. The RD-180 engines are provided by RD Amross, while Aerojet Rocketdyne provides both the RL10 engines and the strap-on boosters used in some configurations. The standard payload fairing sizes are 4 or 5 meters in diameter and of various lengths. Fairings sizes as large as 7.2 m in diameter and up to 32.3 m in length have been considered. The rocket is assembled in Decatur, Alabama and Harlingen, Texas.

Height
59.7 m
Diameter
3.8 m
Stages
2
Recorded launches
19
First flight
2006-01-19

Recorded timing

This is a mission record, not an upcoming calendar appointment.

44 minute windowPublished target
WINDOW OPENS
WINDOW CLOSES

Target ·

The target marker shows its position within the published window. The schedule may change before launch.

Flight timeline

Planned sequence, not live telemetry. Times are relative to the launch target.

  1. T−00:00:02

    Ignition

  2. T+00:00:01

    Liftoff

  3. T+00:00:54

    Max-Q

  4. T+00:01:46

    SRB Separation

  5. T+00:03:14

    Fairing Separation

  6. T+00:04:23

    MECO

Show the full sequence (14 events)
  1. T+00:04:29

    Stage 2 Separation

  2. T+00:04:39

    SES-1

  3. T+00:11:35

    SECO-1

  4. T+00:21:34

    SES-2

  5. T+00:26:55

    SECO-2

  6. T+03:26:00

    SES-3

  7. T+03:29:08

    SECO-3

  8. T+03:32:23

    Payload Separation

Launch site & orbit

Cape Canaveral SFS, FL, USA

The mission in perspective

Launch site & orbit

Explore the launch pad, then pull back to see the shape of the destination orbit.

Understand this orbit
NASA Blue Marble map of Earth's continents and oceans
Representative orbit · accelerated illustrationNo live tracking or simulated ascent. NASA Blue Marble.

Coverage & sources

Links supplied by the mission data provider.
Coverage and times may change.

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