Operational Aspects of Landsat 8 and 9 Geometry

• Published in: Remote sensing (Basel, Switzerland) Switzerland), 2024-01, Vol.16 (1), p.133
• Main Authors: Choate, Michael J., Rengarajan, Rajagopalan, Hasan, Md Nahid, Denevan, Alexander, Ruslander, Kathryn
• Format: Article
• Language: English
• Subjects: Accuracy; Archives & records; Artificial satellites in remote sensing; Calibration; Commissioning; Control equipment; Control systems; Data acquisition; Design; Design and construction; Geometry; Global positioning systems; GPS; Landsat; Landsat 8; Landsat 9; Methods; Operational Land Imager-1; Operational Land Imager-2; Registration; Remote sensing; Reprocessing; Sensors; Space ships; Space vehicles; Spacecraft; Spacecraft attitude control; Thermal Infrared Sensor-1; Thermal Infrared Sensor-2
• ISSN: 2072-4292; 2072-4292
• DOI: 10.3390/rs16010133

Landsat 9 (L9) was launched on 27 September 2021. This spacecraft contained two instruments, the Operational Land Imager-2 (OLI-2) and Thermal Infrared Sensor-2 (TIRS-2), that allow for a continuation of the Landsat program and the mission to acquire multi-spectral observations of the globe on a moderate scale. Following a period of commissioning, during which time the spacecraft and instruments were initialized and set up for operations, with the initial calibration performed, the mission moved to an operational mode This operational mode involved the same cadence and methods that were performed for the Landsat 8 (L8) spacecraft and the two instruments onboard, the Operational Land Imager-1 (OLI-1) and Thermal Infrared Sensor-1 (TIRS-1), with respect to calibration, characterization, and validation. This paper discusses the geometric operational aspects of the L9 instruments during the first year of the mission and post-commissioning, and compares these same geometric activities performed for L8 during the same time frame. During this time, optical axes of the two sensors, OLI-1 and OLI-2, were adjusted to stay aligned with the spacecraft’s Attitude Control System (ACS), and the TIRS-1 and TIRS-2 instruments were adjusted to stay aligned with the OLI-1 and OLI-2 instruments, respectively. In this paper, the L9 operational adjustments are compared to the same operational aspects of L8 during this same time frame. The comparisons shown in this paper will demonstrate that both instruments aboard L8 and L9 performed very similar geometric qualities while fully meeting the expected requirements. This paper describes the geometric differences between the L9 imagery that was made available to the public prior to the reprocessing campaign that was performed using the new calibration updates to the sensor and to ACS and TIRS-to-OLI alignment parameters. This reprocessing campaign of L9 products involved data acquired from the launch of the spacecraft up to early 2023.