ALOS-2
ALOS-2, launched in 2014, continued Japan's radar Earth-observation program with the PALSAR-2 L-band synthetic-aperture radar. It supports disaster response, land monitoring, forestry and measurements of ground deformation.
Object identity
- NORAD ID
- 39766
- COSPAR ID
- 2014-029A
- Operator
- Not listed
- Country
- Not listed
- Launch date
- Not listed
Immediate discovery
Why this satellite matters
Interferometric SAR compares the phase of radar signals from repeated passes. Tiny phase differences can reveal ground movement on the scale of centimeters or less.
Understanding the mission
Science and engineering ideas
Interferometric SAR compares the phase of radar signals from repeated passes. Tiny phase differences can reveal ground movement on the scale of centimeters or less.
Mission
Mission and purpose
The current public orbital catalog identifies this object, but verified mission-specific information may be limited. TransitSatellite will expand this page when authoritative information is available.
- Interferometric SAR compares the phase of radar signals from repeated passes. Tiny phase differences can reveal ground movement on the scale of centimeters or less.
Design
Engineering
Interferometric SAR compares the phase of radar signals from repeated passes. Tiny phase differences can reveal ground movement on the scale of centimeters or less.
Real orbital values
The mathematics
The current two-line element set reports approximately 14.7948 revolutions per day. Dividing 1,440 minutes by that value gives an estimated orbital period of 97.3 minutes.
Period
97.3 min
Representative speed
27,148 km/h
Representative altitude
638 km
Inclination
97.92°
Launch record
Launch and deployment
ALOS-2 launched on 24 May 2014 aboard an H-IIA rocket from Tanegashima Space Center.
Orbit
LEO orbit explained
Low Earth orbit is the region closest to Earth used by most crewed spacecraft, many science missions, Earth-observation satellites, and large constellations. Objects move quickly and commonly complete an orbit in roughly 90 to 130 minutes.
LEO can provide detailed Earth views, lower communications delay, and easier access than higher orbits, but it covers less area per spacecraft and is more affected by atmospheric drag.
Live TransitSatellite experience
See ALOS-2 moving now
Open the live tracker to view its current calculated position, trajectory, orbital information, visibility tools, and Save and Share controls.
Learning
Questions to explore
- What can an orbit tell us before the mission is fully identified?
- Why are stable catalog identifiers important?
Evidence
Sources and data notes
Current identity and orbital elements come from CelesTrak’s public GP data. Calculated orbit values are derived from the current TLE and may change after catalog updates. Mission-history claims are added separately and require authoritative sources.
Catalog updated
Sep 20, 2026, 2:45 AM UTC
Story review
1970-01-01T00:00:00.000Z
