N: 54 S: -54 E: 180 W: -180
Description
The ECOsystem Spaceborne Thermal Radiometer Experiment on Space Station (ECOSTRESS) mission measures the temperature of plants to better understand how much water plants need and how they respond to stress. ECOSTRESS is attached to the International Space Station (ISS) and collects data globally between 52° N and 52° S latitudes.
The ECOSTRESS Swath Attitude and Ephemeris Instantaneous Level 1B Global (ECO_L1B_ATT) Version 3 data product provides both ISS-reported and corrected attitude quaternions and spacecraft ephemeris data. Corrected values are derived by image matching against a global Landsat 7 orthoimagery base layer to improve navigation accuracy. The data are provided in 1 second intervals, and each product file contains vectors from the duration of the orbit.
The ECO_L1B_ATT data product contains 10 data layers: both ISS-reported and corrected variables for attitude, ephemeris, position, velocity, and time, distributed in HDF5 format. These data are used to initiate the geolocation process for ECOSTRESS scenes.
Known Issues
- No spatial query in NASA Earthdata Search: This product does not contain spatial bounding box attributes, so granules cannot be searched by geographic location. Users should search for this data product by orbit number.
- Solar Array Obstruction: Some ECOSTRESS scenes may be affected by solar array obstructions from the ISS, potentially impacting data quality in obstructed pixels. The 'FieldOfViewObstruction' metadata field is reliably populated and accurate for all products generated on or after October 2024, following fixes to the Product Generation Executive (PGE) docker configuration and updates to the L1A_RAW_PIX software. Prior to October 2024, the field was not reliably populated; a list of confirmed affected scenes was maintained and is recommended for verifying historical data.
- Historical acquisition gaps and anomalies (2018–2023): Irrecoverable data loss occurred due to Mass Storage Unit (MSU) failures, resulting in permanent gaps in the observational record where no ECOSTRESS data was acquired. Other early issues, including band 4 striping (Feb 2020), 3-band TES mode limitations (May 2019–April 2023), and noisy data periods (e.g., May–July 2025), have been mitigated through reprocessing, firmware updates, and instrument recovery. Version 3 products incorporate these improvements where data exists and are unaffected by ongoing issues, but the permanent historical gaps remain, and caution is advised for time-series analyses spanning affected periods.
Product Summary
Citation
Citation is critically important for dataset documentation and discovery. This dataset is openly shared, without restriction, in accordance with the EOSDIS Data Use and Citation Guidance.
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File Naming Convention
The file name begins with the Sensor (ECO) followed by the Product Version (v003), Processing Level (L1B), Geophysical Parameter (ATT), Orbit Number (40701), Date and Time of Acquisition designated as YYYYMMDDTHHMMSS (20250909T162218), Build Identifier of product generation software (0713), Product Iteration Number (01), and the Data Format (h5).
Documents
USER'S GUIDE
ALGORITHM THEORETICAL BASIS DOCUMENT (ATBD)
ALGORITHM DOCUMENTATION
DATA PRODUCT SPECIFICATION
DATA QUALITY
Variables
The table below lists the variables contained within a single granule for this dataset. Variables often contain observed or derived geophysical measurements collected from a variety of sources, including remote sensing instruments on satellite and airborne platforms, field campaigns, in situ measurements, and model outputs. The terms variable, parameter, scientific data set, layer, and band have been used across NASA’s Earth science disciplines; however, variable is the designated nomenclature in NASA’s Common Metadata Repository (CMR). Variable metadata attributes such as Name, Description, Units, Data Type, Fill Value, Valid Range, and Scale Factor allow users to efficiently process and analyze the data. The full range of attributes may not be applicable to all variables. Additional information on variable attributes is typically available in the data, user guide, and/or other product documentation.
For questions on a specific variable, please use the Earthdata Forum.
| Name Sort descending | Description | Units | Data Type | Fill Value | Valid Range | Scale Factor | Offset |
|---|---|---|---|---|---|---|---|
| Attitude quaternion | Attitude quaternion, goes from spacecraft to ECI (J2000 Inertial Frame). The coefficient convention used has the real part in the first column. | N/A | float64 | N/A | N/A | N/A | N/A |
| Attitude time_j2000 | Time elements for corrected attitude quaternion | Seconds | float64 | N/A | N/A | N/A | N/A |
| Ephemeris eci_position | Corrected Ephemeris ECI position (J2000 Inertial Frame) | meters | float64 | N/A | N/A | N/A | N/A |
| Ephemeris eci_velocity | Corrected Ephemeris ECI velocity (J2000 Inertial Frame) | m/s | float64 | N/A | N/A | N/A | N/A |
| Ephemeris time_j2000 | Time elements for corrected ephemeris data | Seconds | float64 | N/A | N/A | N/A | N/A |
| Uncorrected Attitude quaternion | Attitude quaternion, goes from spacecraft to ECI (J2000 Inertial Frame). The coefficient convention used has the real part in the first column. This is the reported attitude from the ISS, without correction. | N/A | float64 | N/A | N/A | N/A | N/A |
| Uncorrected Attitude time_j2000 | Time elements for uncorrected attitude quaternion | Seconds | float64 | N/A | N/A | N/A | N/A |
| Uncorrected Ephemeris eci_position | ECI position (J2000 Inertial Frame). This is the reported position from the ISS, uncorrected. | meters | float64 | N/A | N/A | N/A | N/A |
| Uncorrected Ephemeris eci_velocity | Uncorrected Ephemeris ECI velocity (J2000 Inertial Frame) | m/s | float64 | N/A | N/A | N/A | N/A |
| Uncorrected Ephemeris time_j2000 | Time elements for uncorrected ephemeris data | Seconds | float64 | N/A | N/A | N/A | N/A |