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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.

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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°

These are representative calculations derived from current orbital elements, not fixed physical specifications. Altitude and speed change around an elliptical orbit, and predictions change as new orbital elements are published.

Launch record

Launch and deployment

ALOS-2 launched on 24 May 2014 aboard an H-IIA rocket from Tanegashima Space Center.

TransitSatellite does not estimate historical launch weather. Temperature, clouds, wind, holds, and scrub reasons will appear only when supported by traceable historical sources.

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

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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