Launch success with telescope solar panels/sunshade deployed.
Falcon Heavy · Astrophysics


The Nancy Grace Roman Space Telescope is a NASA infrared space telescope with a 2.4 m (7.9 ft) wide field of view primary mirror and two scientific instruments. The Wide-Field Instrument (WFI) is a 300.8-megapixel multi-band visible and near-infrared camera, providing a sharpness of images comparable to that achieved by the Hubble Space Telescope over a 0.28 square degree field of view, 100 times larger than imaging cameras on the Hubble. The Coronagraphic Instrument (CGI) is a high-contrast, small field of view camera and spectrometer covering visible and near-infrared wavelengths using novel starlight-suppression technology. Roman objectives include a search for extra-solar planets using gravitational microlensing, and probing the expansion history of the Universe and the growth of cosmic structure, with the goal of measuring the effects of dark energy, the consistency of general relativity, and the curvature of spacetime.
Launch director verifies go for propellant load
Start of propellant loading in the first stage
Start of liquid oxygen loading in the first stage
Start of propellant loading in the second stage
Start of liquid oxygen loading in the second stage
Start of engine chilling
The onboard computer takes control over the countdown and runs last checks
Launch director verifies go for launch
Fuel tanks are pressurized to flight levels
Start of the engine ignition sequence
First upwards movement of the rocket
Maximum dynamic pressure
Cut-off of the side boosters
Separation of the side boosters
Flip maneuver of the side boosters
Start of the boosters boostback burn
End of the boosters boostback burn
Cut-off of the main engine
Separation of the second stage from the first
First start of the second engine
Separation of the payload fairing
Start of the boosters atmospheric entry burn
End of the boosters atmospheric entry burn
Start of the boosters landing burn
Landing of the boosters
First cut-off of the second engine
Second start of the second engine
Second cut-off of the second engine
Final deployment of the payload from the rocket
Activity appears when ORBITAL observes a change between source records. No historical events are invented.
Launch success with telescope solar panels/sunshade deployed.
Payload deployed.
Liftoff!
Updated launch weather, 70% GO.
Official Webcast by NASA has started
Now targeting Aug 30 at 11:26 UTC
Updated launch weather, 50% GO (launch window per https://x.com/spaceflightnow/status/2093717878302216462).
Now targeting Aug 30 at 11:25 UTC
Updated launch weather, 60% GO.
GO for launch.
Tweaked T-0.
Setting GO.
Added tentative launch time.
NET August 30.
NET late August.
May move up to NET early September.
NET September 28.
NET September.
Adding launch NET October 2026
No changes recorded
Changes are recorded when ORBITAL retrieves data. The detection time may differ from the time the source changed its information.
The Falcon Heavy is a variant of the Falcon 9 full thrust launch vehicle and consists of a standard Falcon 9 rocket core, with two additional boosters derived from the Falcon 9 first stage.
The Nancy Grace Roman Space Telescope is a NASA infrared space telescope based on an existing 2.4 m (7.9 ft) wide field of view primary mirror and carrying two scientific instruments. The Wide-Field Instrument (WFI) is a 300.8-megapixel multi-band visible and near-infrared camera, providing a sharpness of images comparable to that achieved by the Hubble Space Telescope over a 0.28 square degree field of view, 100 times larger than imaging cameras on the Hubble. The Coronagraph Instrument (CGI) is a high-contrast, small field of view camera and spectrometer covering visible and near-infrared wavelengths using novel starlight-suppression technology.
Launch Complex 39A
Kennedy Space Center, FL, USA
Official mission broadcast. Stream availability is controlled by the provider.
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