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ULA Atlas V 551 Amazon Leo (KA-01) - space launch mission detailed information

When is ULA Atlas V 551 Amazon Leo (KA-01)? Launch date 28/APR/2025 — Atlas V 551 rocket launch by United Launch Alliance from Space Launch Complex 41.

ULA Atlas V 551 Amazon Leo (KA-01) launch date, launch time, live countdown, live stream and mission status (Success) — tracked on Space Realm.

ULA Atlas V 551 Amazon Leo (KA-01)

Atlas V 551 rocket used for the Amazon Leo (KA-01) space launch

Atlas V 551

USA flag — Atlas V 551 rocket external-link-icon-img

Status

Success

Date

28 APR 2025

23:01

Mission Overview

Amazon Leo, formerly known as Project Kuiper, is a mega constellation of satellites in Low Earth Orbit that will offer broadband internet access, this constellation will be managed by Kuiper Systems LLC, a subsidiary of Amazon. This constellation is planned to be composed of 3,276 satellites. The satellites are projected to be placed in 98 orbital planes in three orbital layers, one at 590 km, 610 km and 630 km altitude. 27 satellites are carried on this launch.

Rocket

Atlas V 551

Mission Type

Communications

Orbit

Low Earth Orbit

Stages

2

Livestream

watch on source

Rocket Details

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

Launch Mass

573 T

Thrust

12,269 kN

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