Mission Segments
Space
Landsat Next will consist of three identical satellite observatories, equally spaced in orbit to provide the triplet constellation a 6-day revisit of any location on Earth’s land and coastal regions. The entire constellation will be a Category 2, Class B mission with a 5-year design life, where each observatory will be composed of a Class B spacecraft and a Class C instrument suite. The instrument technical performance is not affected by the risk class designation, and the instruments will include elements and mechanisms more typical of Class B instruments to ensure reliability, resiliency, and robustness.
Each Landsat Next observatory will occupy a sun-synchronous orbit at an altitude of 653 kilometers (406 miles), have an inclination of ~98 degrees, and image the ground track at the equator at 10:10 am ± 5 minutes (mean local time at descending node). For each individual observatory to achieve an 18-day temporal revisit based on the field-of-view requirements, the trio will fly a lower altitude than previous Landsat satellites.
Launch
Details of the launch vehicle are not finalized at this point. All three Landsat Next observatories will be on one launch vehicle.
Ground
The Landsat Next ground system will be built on the backbone of previous systems. USGS will build and deliver the ground system, operate the observatories, and process and distribute the data. The Mission Operations Center will be at Goddard Space Flight Center in Greenbelt, Maryland, while the Data Process and Archive System (DPAS) will be at the USGS/EROS facility in Sioux Falls, South Dakota.
WRS-3
Images, or scenes, acquired by the former Landsat missions were cataloged and referenced using previous Worldwide Reference System (WRS) grids (WRS-1 and WRS-2). To accommodate the Landsat Next repeating ground track and global revisit cycle, a new global grid reference system called WRS-3 was established to acquire, catalog, and distribute Landsat Next scenes. Preserving the previous global reference system and heritage view angle geometry was considered less critical to the overall Landsat Next mission architecture, since science applications are increasingly moving from scene- to pixel-based analysis using BRDF-normalized data.
WRS-3 PARAMETER
|
VALUE
|
---|---|
Equatorial Altitude
|
653 km
|
Inclination
|
97.9835 degrees
|
Mean Local Time (Descending Node)
|
10:10 am ± 5 minutes
|
Number of Paths
|
265
|
Number of Rows
|
248
|
Repeat Cycle
|
18 days
|
Descending Node Row
|
60
|
Longitude of Path 001, Row 060
|
-65.2 degrees (65.2 W)
|
Swath Width
|
164 km
|
Along-Track Scene Length
|
168 km
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Scene Size
|
164 km x 168 km
|
Mission Schedule and Lifecycle
Landsat Next is expected to launch in 2031. NASA-managed satellite programs divide a mission lifecycle into distinct phases. Phase A is concept and technology development; Phase B is preliminary design and technology completion; Phase C is final design and fabrication; Phase D is system assembly, integration/testing, and launch readiness; Phase E starts after on-orbit operational checkout and ends at the mission’s operational end. Landsat Next passed Key Decision Point-A on November 29, 2022 and is now in Phase A of mission development.