NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
NEA Scout spacecraft after de-integration from hot box
Opening Thermal Vacuum Chamber V15 to extract hot box containing NEA Scout spacecraft 2 of 2
Opening Thermal Vacuum Chamber V15 to extract hot box 2 of 2containing NEA Scout spacecraft.
Opening Thermal Vacuum Chamber V15 to extract hot box containing NEA Scout spacecraft.
Opening Thermal Vacuum Chamber V15 to extract hot box containing NEA Scout spacecraft.
Removal of hot box containing NEA Scout spacecraft from Thermal Vacuum Chamber V15   1 of 2
Removal of hot box containing NEA Scout spacecraft from Thermal Vacuum Chamber V15 1 of 2
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15 and removal of Optical Witness Samples, (OWS), for analysis
NEA (Near Earth Asteroid) Scout Hot Box – Repress Chamber V-15
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEAR EARTH ASTEROID (NEA) SAIL TEAM PERFORMING A DEPLOYMENT OF THE FLIGHT-LIKE ENGINEERING DEVELOPMENT UNIT SOLAR SAIL. THE SAIL WAS MANUFACTURED AT NEXOLVE (HSV, AL) AND DEPLOYED FOR THE FIRST TIME AT MSFC ON AUGUST 4TH, 2016
NEAR EARTH ASTERIOD SCOUT SOLAR SAIL
NEA (Near Earth Asteroid) Scout Solar Sail, deployed, with team members: Alex Sobey, Andy Heaton, Olive Stohlmann, Leslie McNutt, Tiffany Russell Lockett, Roy Young, Les Johnson, Kevin Sykes, Tom Bryan
Near Earth Asteroid Scout Solar Sail
The Near-Earth Asteroid Scout team prepares their secondary payload for installation in the Space Launch System rocket’s Orion stage adapter at NASA’s Kennedy Space Center in Florida. NEA Scout will be deployed and go to an asteroid after the Orion spacecraft separates from the Space Launch System rocket and heads to the Moon during the Artemis I mission.
Artemis I OSA Secondary Payload Load - NEA Scout and LunarIC
NEOWISE, the asteroid-hunting portion of NASA WISE mission, illustrates the differences between orbits of a typical near-Earth asteroid blue and a potentially hazardous asteroid, or PHA orange. PHAs are a subset of the near-Earth asteroids NEAs.
Edge-on View of Near-Earth Asteroids
NASA ADMINISTRATOR BOLDEN IS BRIEFED ON NEA SCOUT PROGRESS BY TIFFANY RUSSELL
CHARLES BOLDEN BRIEFED BY TIFFANY RUSSELL
NASA ADMINISTRATOR BOLDEN IS BRIEFED ON NEA SCOUT PROGRESS BY ALEX SOBEY
CHARLES BOLDEN BRIEFED BY ALEX SOBEY
NASA ADMINISTRATOR BOLDEN IS BRIEFED ON NEA SCOUT PROGRESS BY LES JOHNSON
CHARLES BOLDEN BRIEFED BY LES JOHNSON
NASA ADMINISTRATOR BOLDEN IS BRIEFED ON NEA SCOUT PROGRESS BY LESLIE MCNUTT
CHARLES BOLDEN BRIEFED BY LESLIE MCNUTT
Miria Finckenor collects Optical Witness Samples and swab samples for analysis to verify that the NEA Scout thermal vacuum bake-out is complete and the chamber is clean.
Miria Finckenor collects Optical Witness Samples and swab sample
The NEA Scout and Lunar IceCube secondary payloads are the first to be installed in the Space Launch System (SLS) rocket’s Orion stage adapter for the Artemis I mission on July 14 at NASA’s Kennedy Space Center in Florida.
Artemis I - OSA Secondary Payload: ARGO, BioS
Between Aug. 20 and 24, near-Earth asteroid (NEA) 2016 AJ193 drifted past Earth at a distance of 2.1 million miles (about 3.4 million kilometers), creating an opportunity for planetary radar to image its surface for the first time since its discovery in 2016. Using the 70-meter (230-foot) Deep Space Station 14 antenna at the Deep Space Network's Goldstone Deep Space Complex near Barstow, California, considerable detail in the asteroid's surface was revealed, including ridges, small hills, flat areas, concavities, and possible boulders. In addition, the radar observations of 2016 AJ193 confirmed that it is about three-quarters-of-a-mile (1.3-kilometers) wide. This series of images show the asteroid rotate (with a period of 3.5 hours) as each radar observation was made.  2016 AJ193 is the 1,001st asteroid to be observed by planetary radar, making its close approach with Earth only seven days after the 1,000th NEA to be observed by radar – asteroid 2021 PJ1, which measures between 65 and 100 feet (20 and 30 meters) wide – approached Earth at a distance of 1 million miles (about 1.7 million kilometers).  https://photojournal.jpl.nasa.gov/catalog/PIA24564
Radar Reveals the Surface of Asteroid 2016 AJ193
Teams worked on the final processing of their payloads that will fly aboard Artemis I. Housed within the Orion stage adapter, the satellites – called CubeSats – are roughly the size of a large shoe box and weigh no more than 30 pounds. Despite their small size, they enable science and technology experiments that may enhance our understanding of the deep space environment, expand our knowledge of the Moon, and demonstrate new technologies that could be used on future missions.
Artemis I OSA Secondary Payload Load - NEA Scout and LunarIC
Teams worked on the final processing of their payloads that will fly aboard Artemis I. Housed within the Orion stage adapter, the satellites – called CubeSats – are roughly the size of a large shoe box and weigh no more than 30 pounds. Despite their small size, they enable science and technology experiments that may enhance our understanding of the deep space environment, expand our knowledge of the Moon, and demonstrate new technologies that could be used on future missions.
Artemis I OSA Secondary Payload Load - NEA Scout and LunarIC
Teams worked on the final processing of their payloads that will fly aboard Artemis I. Housed within the Orion stage adapter, the satellites – called CubeSats – are roughly the size of a large shoe box and weigh no more than 30 pounds. Despite their small size, they enable science and technology experiments that may enhance our understanding of the deep space environment, expand our knowledge of the Moon, and demonstrate new technologies that could be used on future missions.
Artemis I OSA Secondary Payload Load - NEA Scout and LunarIC
Teams prepare the Lunar IceCube before its installation in the Space Launch System rocket Orion stage adapter at NASA’s Kennedy Space Center in Florida. This small satellite will be deployed from the rocket and will orbit the Moon for six months and search for water and ice with an infrared spectrometer.
Artemis I OSA Secondary Payload Load - NEA Scout and LunarIC
Teams worked on the final processing of their payloads that will fly aboard Artemis I. Housed within the Orion stage adapter, the satellites – called CubeSats – are roughly the size of a large shoe box and weigh no more than 30 pounds. Despite their small size, they enable science and technology experiments that may enhance our understanding of the deep space environment, expand our knowledge of the Moon, and demonstrate new technologies that could be used on future missions.
Artemis I OSA Secondary Payload Load - NEA Scout and LunarIC
ISS017-E-005037 (19 April 2008) --- Santorini Volcano, Greece is featured in this image photographed by an Expedition 17 crewmember on the International Space Station. According to scientists, one of the largest volcanic eruptions in the past 10,000 years occurred approximately 1620 BC on the volcanic island of Santorini in the Aegean Sea. This view illustrates the center of Santorini Volcano, located approximately 118 kilometers to the north of Crete (not shown). Prior to 1620 BC, the island of Santorini -- now known as Thera -- had been built up by layers of lava created by overlapping shield volcanoes, and had experienced three significant eruptions that formed overlapping calderas, or collapsed magma chambers. Around 1620 BC, the fourth (and latest) major eruption created the present-day islands and caldera bay of Santorini Volcano. The caldera rim is clearly visible in this image as a steep cliff forming the western shoreline of the island of Thera. Following the 1620 BC eruption, much of the previous island of Santorini was destroyed or submerged. The white rooftops of cities and towns trace the caldera rim on the island of Thera, and overlook the young central islands of Nea Kameni and Palaea Kameni -- both, according to scientists, formed from lava domes and flows that started erupting approximately 1400 years after the last major caldera-forming event. Several of these flows are visible in the image as brown to dark-brown irregular masses forming Nea Kameni (left). The most recent volcanic activity in the Kameni islands occurred in 1950, and included some small explosions and production of lava. The extent of development and location of an airport (upper right) on Thera illustrate the popularity of Santorini Volcano as a tourist destination. Today, volcanic activity is closely monitored by the Institute for the Study and Monitoring of the Santorini Volcano, or ISMOSAV.
Earth Observations taken by the Expedition 17 Crew
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer,  Rick Wilson – Lead Test Engineer
Spacecraft in Gravity Off-load Fixture (GOLF), System Test configuration - Arisa Waddle – Test Engineer, Rick Wilson – Lead Test Engineer
This diagram shows the orbit of binary asteroid Didymos around the Sun. Didymos consists of a large, nearly half-mile-wide (780-meter-wide) asteroid orbited by a smaller, 525-foot-wide (160-meter-wide) asteroid, or moonlet. Didymos' orbital path around the Sun is shown as the thin white ellipse and Earth's orbit is the thick white line. In the background are the orbits for 2,200 other known potentially hazardous asteroids.  A potentially hazardous asteroid is classified as an asteroid wider than about 460 feet (140 meters) with an orbit that brings it within 5 million miles (8 million kilometers) of Earth's orbit.  Didymos' smaller asteroid is the target of NASA's Double Asteroid Redirect Test (DART) mission. The DART spacecraft is a kinetic impactor designed to collide with the moonlet to see how its orbit around the larger asteroid will be changed by the impact. The outcome of this mission will help NASA determine whether the method could be used to modify the trajectory of an asteroid should one threaten Earth in the future. Didymos is not a danger to our planet.  This orbital diagram was produced by the Center for Near Earth Object Studies (CNEOS), which is managed by NASA's Jet Propulsion Laboratory in Southern California. CNEOS characterizes every known near-Earth asteroid (NEA) orbit to improve long-term impact hazard assessments in support of NASA's Planetary Defense Coordination Office (PDCO).  https://photojournal.jpl.nasa.gov/catalog/PIA24565
The Orbit of Asteroid Didymos
This figure represents the 1,000th near-Earth asteroid (NEA) to be detected by planetary radar since 1968. Being only 65 to 100 feet (20 to 30 meters) wide, asteroid 2021 PJ1 was too small to be imaged in any detail, but the powerful 70-meter (230-foot) Deep Space Station 14 (DSS-14) antenna at the Deep Space Network's Goldstone Deep Space Complex near Barstow, California, was able to measure the Doppler frequency of the radio waves that reflected off the object's surface. The data was recorded for 16 minutes between 2:26 p.m. and 2:42 p.m. PDT on Aug. 14, 2021.      The figure shows radar echo signal strength on the vertical axis versus Doppler frequency (in units of hertz, or Hz) on the horizontal axis. The strong spike at a value of minus 70 Hz is the reflected signal (or "echo") from 2021 PJ1; the other, smaller spikes are receiver noise, which is like the static on an AM radio if there aren't any nearby stations.      Using this information, scientists at NASA's Jet Propulsion Laboratory in Southern California could more accurately calculate the asteroid's velocity, its distance from Earth and its future motion around the Sun.      These observations used a prediction – known as an "ephemeris" – that had relatively large uncertainties because the asteroid had been discovered only a few days earlier. If the original prediction had been perfect, the radar echo would appear at zero Hz. The fact that the radar echo is at minus 70 Hz indicates a correction could be made to the predicted velocity of minus 2.7 miles per hour (minus 1.2 meters per second). This measurement also reduced the uncertainty in the asteroid's distance from Earth from 1,300 miles (2,100 kilometers) to 5.2 miles (8.3 kilometers) – a reduction of a factor of about 250.  https://photojournal.jpl.nasa.gov/catalog/PIA24563
The Doppler Spike of Asteroid 2021 PJ1