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SAOCOM 1A

SAOCOM 1A is an Argentine L-band radar Earth-observation satellite launched in 2018. It is designed especially for soil-moisture and disaster-related applications and works in coordination with other radar missions.

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Object identity

NORAD ID
43641
COSPAR ID
2018-076A
Operator
Not listed
Country
Not listed
Launch date
Not listed

Immediate discovery

Why this satellite matters

Longer-wavelength L-band radar penetrates vegetation more effectively than shorter wavelengths in many conditions, making it useful for soil and biomass studies.

Understanding the mission

Science and engineering ideas

Longer-wavelength L-band radar penetrates vegetation more effectively than shorter wavelengths in many conditions, making it useful for soil and biomass studies.

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.

  • Longer-wavelength L-band radar penetrates vegetation more effectively than shorter wavelengths in many conditions, making it useful for soil and biomass studies.

Design

Engineering

Longer-wavelength L-band radar penetrates vegetation more effectively than shorter wavelengths in many conditions, making it useful for soil and biomass studies.

Real orbital values

The mathematics

The current two-line element set reports approximately 14.8215 revolutions per day. Dividing 1,440 minutes by that value gives an estimated orbital period of 97.2 minutes.

Period

97.2 min

Representative speed

27,164 km/h

Representative altitude

630 km

Inclination

97.89°

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

SAOCOM 1A launched on 7 October 2018 aboard a Falcon 9 from Vandenberg Air Force Base.

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 17, 2026, 1:04 AM UTC

Story review

1970-01-01T00:00:00.000Z